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#1 Re: Science, Technology, and Astronomy » Manufacturing in Space » Yesterday 19:16:51

That's good as I recall the first crystal formation failed to get purity due to the vibrations within the ship.

#2 Re: Human missions » Starship is Go... » Yesterday 19:10:23

Why Elon Musk now says it would be a 'distraction' for SpaceX to go to Mars this year

SpaceX is unlikely to attempt a Mars mission in 2026 after all, according to CEO Elon Musk, marking a setback in his plans to colonize the planet.

“It would be a low-probability shot and somewhat of a distraction,” Musk told entrepreneur Peter Diamandis in a podcast recorded in late December and published this week.
In September 2024, Musk discussed SpaceX’s plans to send an uncrewed Starship rocket to Mars this coming year. At the time, Musk said the mission would test how reliably SpaceX could land its vehicles on the planet’s surface. If things went well, he estimated SpaceX could send crewed missions as soon as 2028.

But Musk has dialed back his optimism over the past year. In May, he gave his company a 50% chance of being ready for a launch in late 2026, which would coincide with a narrow window that occurs every two years when Mars and Earth align. A few months later, he said the uncrewed flight would “most likely” happen in 2029.

August 2025, Musk said there was a “slight chance” of a Starship flight to Mars in November or December 2026 crewed by Optimus, the humanoid robots being developed by Tesla “A lot needs to go right for that.”

A mission to Mars hinges on SpaceX being capable of refueling Starship’s upper stage in orbit, a complicated task that Musk told Diamandis could be achieved toward the end of 2026. Accomplishing orbital refueling is also crucial for SpaceX to complete a recently reopened contract to carry NASA astronauts to the moon.

SpaceX was on track to demonstrate its process — which involves launching tanker versions of Starship into orbit — in 2025, a NASA official said the year before. But the company missed that target and now plans to attempt its first orbital-refueling demonstration between Starship vehicles in June, according to internal documents viewed by Politico.

SpaceX, which is now developing the third generation of the reusable 404-foot Starship rocket, has also had difficulty testing its vehicle. Its first three flights of 2025 were failures, while the remaining two launch attempts were much more successful. The next iteration of Starship will be a “massive upgrade” over its predecessor, Musk has said.SpaceX was on track to demonstrate its process — which involves launching tanker versions of Starship into orbit — in 2025, a NASA official said the year before. But the company missed that target and now plans to attempt its first orbital-refueling demonstration between Starship vehicles in June, according to internal documents viewed by Politico.

SpaceX, which is now developing the third generation of the reusable 404-foot Starship rocket, has also had difficulty testing its vehicle. Its first three flights of 2025 were failures, while the remaining two launch attempts were much more successful. The next iteration of Starship will be a “massive upgrade” over its predecessor, Musk has said.

In addition to preparing for Mars and lunar missions, SpaceX dominates the commercial launch industry and runs a successful satellite-internet business. It plans to go public later this year in what could be a record-breaking listing that could help fund its plans for Starship as well as for space-based data centers.

Although SpaceX probably won’t be headed to the red planet in 2026, twin spacecraft will make the journey this year. Blue and Gold, a pair of satellites developed by Rocket Lab were launched into space last November by Amazon founder Jeff Bezos’s Blue Origin to fulfill NASA’s Escapade mission.

The spacecraft are expected to attempt a trans-Mars injection engine burn in November 2026 and arrive at the planet in September of next year, according to NASA. The satellites will be operated by the Space Sciences Laboratory at the University of California, Berkeley, and will gather data that could help humans land on or even settle Mars.

This guy might be the first
tesla_optimus_gen_2_humanoid_robot_white_002.jpg

#3 Re: Exploration to Settlement Creation » Starship repurposed to make or build what we need » Yesterday 18:53:11

I found images of the building of the super dome

5d1523381783d.image.jpg?resize=736%2C500

5j8g379dme261.png?auto=webp&s=19ffa6d6918a7f9639de053da572ba4b59a40ebb

nfl_a_superdome_300.jpg

Scalable structure that could be made from the cannibalized starships, cut and bend to shape.

#4 Re: Meta New Mars » Housekeeping » Yesterday 18:30:35

DreamHost experienced a major Denial of Service (DoS/DDoS) attack targeting its DNS servers in August 2017, which caused widespread outages for many of its customers' websites, including the Newmars forum. The attack overwhelmed DreamHost's infrastructure, making websites inaccessible by preventing them from resolving their IP addresses.
Details of the Incident
Nature of the Attack: The attacks were a large-scale Distributed Denial of Service (DDoS), which is designed to knock websites offline by overloading servers with malicious traffic.
Target: The primary targets were DreamHost's DNS (Domain Name System) servers (ns1, ns2, and ns3.dreamhost.com), which are essential for directing internet traffic to the correct websites.
Impact on Newmars Forum: As the Newmars forum likely used DreamHost's DNS services, it was one of the many sites affected by the resulting downtime.
DreamHost's Response: DreamHost acknowledged the powerful DDoS attack and worked to mitigate the issue. The company's acceptable use policy explicitly prohibits any activity that results in their servers becoming the target of a DoS attack.
Current Status
The 2017 incident was resolved a short time after it occurred. If you are experiencing current issues with the Newmars forum, it is recommended to check the DreamHost Status page for any ongoing incidents

he query refers to a specific discussion or incident on a forum related to the "New Mars Image Server" and a potential phpBB3 denial of service issue at DreamHost.
Based on search results, the issue appears to be a forum-specific problem where bots/crawlers caused high server load, which the site administrator addressed by blacklisting IP addresses, rather than a large-scale attack on DreamHost's infrastructure. DreamHost has, however, experienced large-scale, unrelated DDoS attacks targeting their DNS servers in the past (e.g., in August 2017).
Details of the Incident
Nature of the Issue: The problem at the "New Mars Image Server" (newmars.com) was likely caused by automated bots or scrapers, rather than a malicious, coordinated denial-of-service attack. These bots generated excessive traffic and server load by repeatedly requesting non-existent files or creating new sessions, leading to service interruptions.
Mitigation: The forum administrator implemented a fix by identifying specific bot user-agent strings and blacklisting problematic IP addresses, which successfully stopped the issue. They also discussed implementing Q&A CAPTCHAs to prevent spam registrations and closing the board during maintenance as prevention methods.
DreamHost's Stance: DreamHost prohibits all forms of denial of service attacks and related activities under its Acceptable Use Policy. If abuse is detected, they may take action to secure the account, including suspension or termination of service.
General Guidance
If you are experiencing similar issues on a phpBB board hosted by DreamHost:
Check logs: Review your access logs for unusual activity, especially repetitive requests from specific IP addresses or abnormal user-agent strings.
Configure phpBB settings: Utilize phpBB's built-in spam prevention tools, such as Q&A CAPTCHAs, and configure spider/robot settings to handle legitimate bots efficiently.
Update software: Ensure your phpBB installation, themes, and any plugins are kept up to date to patch known vulnerabilities that could be exploited to cause a DoS.
Contact Support: If you suspect an ongoing attack affecting your server performance, you should contact DreamHost support immediately. They can help identify the cause and potentially whitelist ModSecurity rules or apply server-level mitigation if necessary

#5 Re: Meta New Mars » Housekeeping » Yesterday 18:26:31

Denial of service?

A website crash due to "too many connections" in the log file typically means your database server has reached its maximum connection limit. This can be caused by unoptimized code, connection leaks, or a sudden spike in traffic.

Here are the steps to diagnose and resolve the issue:
Immediate Stabilization
Restart the Application/Database Server: The quickest way to clear all current connections and restore service is to restart your web application or database server. This immediately closes all existing connections.
Manually Kill Idle Connections: If you have administrative access (e.g., via the MySQL command line), you can connect and terminate "sleeping" or idle processes.

Log in to MySQL: mysql -u root -p
View active connections: SHOW PROCESSLIST;
Kill specific connections: KILL <process_id>; (replace <process_id> with the actual ID from the list)
Temporarily Increase the Connection Limit: To prevent the crash from recurring immediately, you can temporarily increase the max_connections variable.
In the MySQL client, run: SET GLOBAL max_connections = [desired new number];
This is a temporary fix and will revert on the next server restart unless made permanent in the configuration file.

Long-Term Solutions
Identify the Root Cause: The primary goal is to determine why so many connections are being opened or staying open.
Check logs for slow queries: Use the SHOW PROCESSLIST; command to identify any long-running queries that are tying up connections.
Enable the slow query log in your MySQL configuration file to help pinpoint inefficient queries.

Optimize Application Code and Queries:
Ensure connections close properly: Verify your application code closes database connections after use. Many modern frameworks and languages have features like context managers (Python) or specific close functions ($conn->close() in PHP) to handle this.
Use connection pooling: Implement a connection pool in your application. This reuses a set number of open connections instead of opening a new one for every request, which is much more efficient.

Adjust Server Configuration (Permanently):
Edit your MySQL configuration file (commonly /etc/my.cnf or /etc/mysql/my.cnf).
Under the [mysqld] section, add or update the max_connections line: max_connections=[new value].
Consider reducing the wait_timeout setting to automatically close idle connections more quickly (e.g., to 300 seconds or 5 minutes, down from the default 8 hours).

Restart the MySQL service for these changes to take permanent effect.
Monitor and Scale:
Set up monitoring tools (e.g., Nagios, Prometheus) to track connection usage, CPU/memory usage, and other performance metrics.
If you consistently experience high traffic and the above optimizations aren't enough, you may have outgrown your current hosting plan (e.g., shared hosting) and should consider upgrading to a Virtual Private Server (VPS) or a dedicated server, or implementing load balancing.
Use a Content Delivery Network (CDN) to offload static assets (images, CSS, JS), which reduces the load on your primary server

#6 Re: Exploration to Settlement Creation » Project Designing for Mars » Yesterday 16:28:55

For a Martian habitat at 0.5 bar (significantly higher than Mars's ~0.006 bar average), spherical or cylindrical shapes are optimal for a stainless steel structure, as they efficiently contain internal pressure, with cylindrical shapes often favored for practical construction and use with regolith shielding, using tension members to handle stress, similar to pressurized vessels on Earth.

Why These Shapes?
Spherical: A sphere distributes stress equally in all directions, making it structurally ideal for holding internal pressure against a vacuum or low external pressure.

Cylindrical: Cylinders (especially with domed ends) are practical for larger volumes, offer better usable floor space, and can be buried or covered with Martian soil (regolith) for radiation shielding without collapsing.

Structural Considerations for 0.5 Bar (50 kPa)
Pressure Difference: A habitat at 0.5 bar (50 kPa) has a substantial pressure difference from the Martian surface (around 0.6 kPa), requiring robust structures.

Stainless Steel: While good for strength, stainless steel is heavy, making it costly to transport; however, it's excellent for withstanding pressure.

Tension: The primary force is outward tension. Structural members (like steel bands) wrapped around cylindrical habitats help contain this.
Design Concepts

Buried Cylinders: Building cylindrical habitats within trenches and covering them with regolith provides shielding from radiation and micrometeoroids, using the soil's weight to help counteract the internal pressure, notes Marspedia and NIH.

Domes: Dome-shaped structures (hemispherical) are also efficient for pressure containment, as studied by NASA.

In essence, think of large, pressurized tanks – spheres and cylinders are the best shapes for holding pressure, and adding regolith makes them even more effective Martian habitats

#7 Re: Exploration to Settlement Creation » Project Designing for Mars » Yesterday 16:27:10

Fishbone theory, or the Fishbone Diagram (also known as an Ishikawa Diagram or Cause-and-Effect Diagram), is a visual tool for root cause analysis that maps out potential causes of a problem in a fish-skeleton-like structure, helping teams brainstorm, categorize, and identify underlying issues, not just symptoms, for better problem-solving in quality control and management. The problem is the "head," and major causes branch off the "backbone" as "ribs," with sub-causes extending further, revealing hidden linkages and process bottlenecks for future improvements.

Key Components & Structure
Head (Right): The specific problem or defect being analyzed.

Backbone (Horizontal Line): Connects the head to the causes.
Major Causes (Ribs): Large bones branching off the backbone, representing broad categories (e.g., People, Method, Machine, Material,

Measurement, Environment).
Root Causes (Smaller Bones): Sub-branches extending from the major causes, detailing specific reasons within each category.

How it Works (The Process)
Define the Problem: Clearly state the issue in the "head".
Identify Categories: Determine major areas where causes might originate (e.g., the 6 Ms: Methods, Machines, Materials, Manpower, Measurement, Mother Nature/Environment).
Brainstorm Causes: For each category, list all possible causes, adding them as smaller bones.
Deep Dive: Use techniques like the "5 Whys" on sub-branches to find deeper root causes.

Benefits & Uses
Visualizes complex problems: Makes it easy to see all potential causes at once.
Promotes shared understanding: Helps teams build consensus on a problem.
Focuses on root causes: Moves beyond symptoms to find the source of issues.
Used in many fields: Popular in manufacturing, healthcare, quality management, and product development

#8 Re: Exploration to Settlement Creation » Project Designing for Mars » Yesterday 16:27:03

Mars in-situ regolith mining equipment involves robotic excavators (like RASSOR/Razer), drilling/microwave probes for volatiles, and processing units for extracting water, metals (iron/steel), and oxygen, using systems like Solid Oxide Electrolysis Cells (SOEC) (MOXIE heritage) and 3D printing for construction materials, with key technologies focusing on automation, heat recycling, and handling abrasive Martian dust for ISRU (In-Situ Resource Utilization).

Key Equipment & Technologies
Excavation & Collection:
Robotic Excavators/Rovers: Systems like RASSOR 2.0 and Razer use counter-rotating drums or buckets for digging in low gravity, designed for high volume and autonomous operation.
Microwave Probes: Non-excavation method to heat subsurface ice, turning it into vapor for collection, reducing mass/cost of heavy machinery.

Processing & Extraction (ISRU):
Water/Volatiles: Extraction from regolith via microwave sublimation or drilling, followed by purification (membranes, distillation) and electrolysis to produce hydrogen (fuel) and oxygen (life support).
Metals & Oxygen: Systems (like MMOST) use electrolysis and reduction processes (e.g., using H₂/CO) to extract iron, steel, and oxygen from iron oxides in regolith.
Sifting/Refining: Machinery to achieve optimal particle size for construction aggregates, often involving heating and mixing with binders like sulfur.

Manufacturing & Construction:
3D Printers: Use processed regolith (sintered, mixed with binders) to build structures, reducing reliance on Earth-imported materials.
Sulfur Concrete Units: Heated mixers (pugmills) to combine regolith aggregate with molten sulfur (around 120°C) for bricks.
Key Processing Units:
Solid Oxide Electrolysis Cells (SOEC): Efficiently split water and CO₂ into constituent gases (H₂, O₂, CO) for chemical processing.
Heated Mixers/Kilns: For creating construction materials like sulfur concrete or sintering regolith.
Challenges & Considerations
Automation: Mining must be fully robotic and autonomous due to distance and communication delays.
Abrasion: Martian dust is highly abrasive, requiring robust seals and durable components.
Power & Logistics: Requires reliable, renewable power and efficient transport/storage systems.
High-Fidelity Simulants: Accurate testing relies on materials like MGS-1C (clay-rich) and MGS-1S (sulfate-rich) to mimic real Martian conditions.

Example System (Conceptual)
An integrated system might include a Razer excavator, feeding a processing unit that uses SOECs and heat recycling to produce oxygen, water, and metal powders, with a 3D printer using these materials to build habitats.

#9 Re: Exploration to Settlement Creation » Project Designing for Mars » Yesterday 16:26:52

In-situ (Latin for "on-site" or "in its original place") in the context of Mars construction refers to the practice of using local Martian resources, rather than transporting all materials and equipment from Earth. This is officially called In-Situ Resource Utilization (ISRU).

The core concept is "living off the land" to drastically reduce the enormous cost and logistical challenge of sending supplies across vast distances from Earth.

The idea that you would have no equipment at all is generally not feasible; some minimal, specialized equipment and robotic systems would be sent from Earth to act as the initial "factories" and "builders". How ISRU Addresses the "No Equipment" Constraint (Relatively) The goal is to minimize the mass and volume of material that must be launched from Earth, not to eliminate equipment entirely. Specialized, compact, and often autonomous, equipment would be sent first to leverage local materials.

The strategy involves: Sending minimal, critical machinery: Instead of sending heavy raw materials like concrete or steel beams, lightweight robotic equipment, 3D printers, and processing hardware are sent.

Utilizing local materials: The robots would use abundant Martian resources, primarily the soil (regolith) and atmosphere, to produce usable products.

Automated construction: The construction process would likely be managed by autonomous or semi-autonomous robots before humans arrive, allowing for the creation of habitats and infrastructure in advance.

Examples of In-Situ Resources for Construction With specialized equipment,
Mars offers several resources: Regolith (Martian soil): This can be used as a primary building material. Processes like sintering (fusing with heat) or mixing with binding agents (like an epoxy or sulfur) can create bricks, ceramics, and concrete-like structures for radiation shielding and general construction..

Water ice: Found below the surface, water is a critical resource. Once extracted, it can be used for life support (drinking water, growing food), split into hydrogen and oxygen (for breathing air and rocket propellant), or used in industrial processes.Atmospheric \(\text{CO}_{2}\): The Martian atmosphere is mostly carbon dioxide. Equipment like the MOXIE experiment on the Perseverance rover can extract oxygen from the atmosphere for life support and as an oxidizer for rocket fuel.

Basalt: Basaltic rocks are abundant and can be processed into glass or glass fibers, which have good insulating properties and can be used for construction. Essentially, "in-situ construction" is the practice of building with what you have on Mars, which is crucial for long-term sustainability and survival when resupply from Earth is nearly impossible

#10 Re: Exploration to Settlement Creation » Project Designing for Mars » Yesterday 16:25:09

Mars settlement projects, like SpaceX's vision, progress through phases: pre-settlement (outposts), in-settlement (permanent bases), and post-settlement (self-sufficient society), aiming for crewed landings in the late 2020s/early 2030s and self-sufficiency by mid-century, requiring massive initial cargo (Starships carrying 100+ tons) for habitats, life support, and resource utilization (ISRU) like water and fuel production from Martian air and ice, with the ultimate goal of a large, self-sustaining population.
Phases of Development (Conceptual)
1.    Pre-Settlement (Exploration & Outpost)
•    Focus: Robotic missions, establishing basic infrastructure, resource identification (water ice, minerals).
•    Key Tech: Advanced rovers, ISRU (In-Situ Resource Utilization) for oxygen/methane (fuel/air).
•    Timeline: Current robotic exploration, early cargo missions (late 2020s).
2.    In-Settlement (Permanent Base)
•    Focus: First human landings, establishing initial habitats, expanding resource production (ISRU, agriculture), reducing Earth dependency.
•    Key Tech: Habitable modules, power systems, water processing, basic manufacturing.
•    Timeline: First crewed landings (early 2030s), developing permanent presence.
3.    Post-Settlement (Self-Sufficient Society)
•    Focus: Large-scale population, full industrialization, economic self-sufficiency, cultural development.
•    Key Tech: Advanced manufacturing, large-scale life support, robust local economy, potential for terraforming elements.
•    Timeline: Decades-long process, aiming for self-sufficiency by 2050+.
Timeline & Mass Estimates (SpaceX Example)
•    Early Missions (2020s-2030s): Cargo & Crew via Starship (100+ tons capacity).
•    Cargo: Essential for habitats, initial supplies, ISRU equipment.
•    Crew: Small groups (4-10+), increasing over time.
•    Self-Sufficiency: Goal by 2050, requiring a million people using numerous Starships over many launch windows (every ~26 months).
Mass Requirements & Challenges
•    High Mass: Water, air (oxygen/nitrogen), fuel, food, equipment, habitats.
•    ISRU Critical: Extracting water ice and using atmospheric CO2 for oxygen and methane fuel (CH4) is essential to reduce launch mass from Earth.
•    Example: Water is heavy; a Starship (100 tons payload) could carry enough water for 20 people for years, but continuous resupply is needed.
In essence, Mars settlement requires a phased approach, leveraging current tech like Starship for massive cargo delivery, transitioning from outposts to permanent bases, and finally, fostering self-sufficiency through local resource utilization to support a growing population

#11 Re: Exploration to Settlement Creation » Project Designing for Mars » Yesterday 16:24:48

Mars settlement projects typically progress through phases from initial robotic exploration and small outposts (Pre-settlement) to permanent, growing settlements with developing infrastructure (In-settlement), culminating in self-sufficient, potentially terraformed societies (Post-settlement), focusing first on establishing basic life support, resource utilization (ISRU), energy, and habitats before expanding to a city-like presence with economic independence. Key stages involve robotic reconnaissance, crewed landings, building propellant plants, establishing habitats, developing local agriculture, mining, and transitioning to self-sufficiency, requiring advances in transportation, closed-loop life support, and energy systems.
Key Phases & Stages
1.    Pre-Settlement (Robotic & Early Outpost):
•    Robotic Reconnaissance: Detailed surveys, sample collection (e.g., Perseverance), testing technologies for fuel/oxygen production from the atmosphere.
•    Cargo Pre-Deployment: Sending autonomous cargo, including fuel production equipment, before human arrival.
•    First Crewed Missions: Establishing a rudimentary base, completing the propellant plant for return fuel, and testing life support.
2.    In-Settlement (Permanent & Growing Colony):
•    Infrastructure Development: Building habitats, mining water, growing crops, creating power systems (solar/nuclear).
•    Resource Utilization (ISRU): Extracting and processing Martian resources (water, metals, minerals) for construction and fuel.
•    Population Growth: Increasing crew sizes, developing a local economy, and establishing governance.
3.    Post-Settlement (Self-Sufficiency & Beyond):
•    Industrial Independence: Scaling up mining, manufacturing (3D printing, metals, plastics) to reduce Earth reliance.
•    Societal Development: Growing into towns/cities, developing unique Martian culture, governance, and potentially independent political structures.
•    Terraforming (Long-Term): Modifying the environment to create breathable air and habitable zones, a highly speculative long-term goal.
Key Technologies & Goals
•    Transportation: Reliable, efficient Earth-Mars transport (e.g., SpaceX Starship).
•    Life Support: Perfecting closed-loop systems for air, water, and food.
•    Energy: Sustainable power generation (solar, nuclear).
•    ISRU: Water extraction, atmospheric processing for fuel/oxygen, material processing.
•    Habitats: Durable, radiation-shielded shelters (surface and underground)

#12 Re: Exploration to Settlement Creation » Project Designing for Mars » Yesterday 16:24:16

Project design phases generally move from understanding the problem to creating detailed solutions, often covering Programming/Pre-Design, Schematic Design, Design Development, Construction Documents, Bidding, and Construction Administration, though models vary (like the AIA's 5 phases or broader project management cycles). Key stages define scope, develop concepts, produce technical drawings, select builders, and oversee building, ensuring a structured path from idea to reality.
Here's a common breakdown, blending architectural and project management steps:
1.    Programming/Pre-Design (Problem Seeking): Define project goals, needs, budget, site analysis, and scope.
2.    Schematic Design (Concept): Develop broad concepts, sketches, and basic layouts to explore possibilities.
3.    Design Development (Refinement): Flesh out the chosen schematic design with materials, systems, and detailed plans.
4.    Construction Documents (Technical Drawings): Create detailed blueprints and specifications for construction.
5.    Bidding/Negotiation: Solicit and select contractors.
6.    Construction Administration (Building): Oversee the building process, ensuring it matches the design.
Variations & Other Models:
•   
Engineering:

Includes research, feasibility, concept generation, detailed design, and production planning.
•   
Design Thinking:

Focuses on empathy, defining problems, ideating, prototyping, and testing (Discover, Define, Develop, Deliver).
•   
Project Management Lifecycle:

Broader stages like Initiation, Planning, Execution, Monitoring & Control, and Closure.
No matter the model, the goal is to break a complex project into manageable steps, moving from abstract ideas to concrete results

#13 Re: Exploration to Settlement Creation » Project Designing for Mars » Yesterday 16:23:55

Project design concepts are the foundational ideas, principles, and high-level plans guiding a project, defining its goals, structure, and key features before detailed planning, using visuals like flowcharts and mood boards to align stakeholders on the 'why' and 'what,' ensuring a shared vision for success. Key elements include defining outcomes, identifying stakeholders, exploring options (like sustainability or accessibility), and establishing success criteria, serving as the blueprint for later execution.
Core Components of Project Design Concepts
•    Goals & Objectives: What the project aims to achieve (e.g., "sleek and minimalist" for a phone).
•    Target Audience & Problem: Who it's for and the problem it solves.
•    Scope & Deliverables: What's included and what will be produced (e.g., sketches, prototypes, reports).
•    Guiding Principles: Overarching ideas like sustainability, accessibility, or efficiency.
•    Visuals & Mood Boards: Mood boards, sketches, flowcharts to convey aesthetics and process.
How They Work
1.    Early Stage: Happens before detailed planning or charter development.
2.    Blueprint: Creates a broad overview (the "what" and "why").
3.    Exploration: Involves generating and evaluating multiple design options.
4.    Stakeholder Alignment: Gets buy-in by presenting choices and setting expectations early.
Examples of Design Principles & Concepts
•    Product: "Safe and reliable" (car) or "Intuitive user experience" (app).
•    Architecture: Integrating local culture, sustainability, or maximizing natural light.
•    Process: Using Agile principles or a specific project management methodology
In essence, a project design concept is the strategic "big picture" that transforms abstract goals into a tangible vision, guiding the entire project from its inception to successful completion.

#14 Exploration to Settlement Creation » Project Designing for Mars » Yesterday 16:23:34

SpaceNut
Replies: 8

Project design is the crucial early phase of outlining a project's "why" and "what"—defining goals, scope, resources, deliverables, and success criteria before detailed planning—to create a strategic blueprint for stakeholders, often using visuals like flowcharts to align teams and guide execution. It establishes the conceptual foundation, differing from detailed project planning which focuses on "how" tasks get done.
Key components
•    Goals & Objectives: What the project aims to achieve (SMART goals are ideal).
•    Scope & Deliverables: Boundaries of the project and tangible outputs.
•    Methodology & Strategy: High-level approach and chosen processes.
•    Resources & Budget: People, tools, budget estimates, and constraints.
•    Success Criteria & KPIs: How success will be measured.
•    Risks: Potential issues and mitigation strategies.
Purpose
•    Alignment: Gets everyone (team, stakeholders) on the same page.
•    Foundation: Creates a clear, agreed-upon path before detailed work begins.
•    Visualization: Uses tools (Gantt, Kanban) to make strategy transparent.
•    Buy-in: Secures stakeholder approval for the overall direction.
Process steps (simplified)
1.    Define the core problem/opportunity.
2.    Establish clear goals and SMART objectives.
3.    Identify key deliverables and success metrics.
4.    Map out required resources and budget.
5.    Identify potential risks and constraints.
6.    Create visual aids (flowcharts, mockups) to communicate the design.
7.    Get stakeholder feedback and approval.
Project design provides the strategic "why" and "what," leading into the detailed "how" of project planning, with outputs like project charters and plans built upon this initial framework

#15 Re: Not So Free Chat » NASA's new leader makes his priorities clear on day one » Yesterday 15:35:38

kbd512 wrote:

I would be remiss if I did not mention the role that NASA's and DOE's partnership programs as the genesis for the commercialization of a lot of these lab curiosities.  Science for its own sake still matters, but so does directed science, aka "engineering", aimed at solving real world problems.  NASA helps industry develop the basic "know-how" to retire risk to begin to apply aerospace technologies to the ordinary everyday world that the majority of us inhabit.

Something that others seem to be forgetting when they look at political power, control and funding.

Part of why the locations of of nasa offices and others that do these things.

#16 Re: Not So Free Chat » Politics » Yesterday 15:22:03

What only a 3 way split???

#17 Re: Human missions » Interview on Fox News with Jared Isaacman » Yesterday 15:16:49

original is in the not so free chat due to politics influence this position as does the others in the senate and house plus the states that have business within them.
So lets stay focused on the interview if possible.

#18 Re: Life support systems » Power generation on Mars » Yesterday 15:14:10

Re-read the quote possible power sources as those are all different for how they are configured and while they give power output you will still need to build converting systems to match the devices that you are powering.

Some will require transformers for step-up and some for down before being made use of.

Think about you computer and you cellphone they both have battery but are they the same size in voltage or power. Yes they have converting transformers and circuitry to interface back to you outlet but they do not conform in any other way.

The cables outside the controlled temperatures of a garage or dome will need different specifications as the cold will make some materials brittle.

So no there is no one forced standard

So the number of watts for creation is not even known?
No list of equipment to make use of those watts?
How much is to be fore personal use?
No list of stuff needing heavy load powered versus items needing next to nothing?

Each building and sections there in are going to needed specifics to solve to what each will need to have configured for use and connection layout.

#19 Re: Life support systems » Power generation on Mars » Yesterday 14:50:53

They are earth safety standards for consumer use...

The specifics are based on wiring diagramming of how the power is to be used which is from the interface circuit breaker box system that you should be aware of.

For a Mars garage, power systems need reliability in dust and cold, likely combining solar arrays with advanced batteries (like Lithium-ion or supercapacitors) for peak loads and consistent energy, supplemented by Radioisotope Thermoelectric Generators (RTGs) or future Nuclear Fission Reactors for baseline power, especially during dust storms and night, alongside energy storage and distribution systems (PMAD) to manage variable demands for tools and habitat functions.
Primary Power Sources
Solar Arrays (Photovoltaics): Efficient when sunlight is available but challenged by dust accumulation and reduced intensity during Martian winter/storms, requiring regular cleaning.
Radioisotope Thermoelectric Generators (RTGs): Use natural decay of plutonium to generate continuous heat and electricity, providing reliable, long-term power independent of sunlight, excellent for baseline needs.
Nuclear Fission Reactors: For larger, sustained power needs (like industrial processes or larger habitats), small fission reactors offer high power output but require significant shielding for radiation.
Energy Storage & Management
Batteries: Rechargeable lithium-ion batteries (like those used on rovers) handle peak power demands, while advanced alternatives like graphene supercapacitors offer faster charging and wider temperature tolerance.
Power Management & Distribution (PMAD): Essential systems to convert, condition, and distribute power from sources to loads, handling start-up, shutdown, and dynamic events.
Supporting Technologies
Waste Heat Utilization: Nuclear systems produce excess heat, which can be converted to electricity or used for habitat/regolith heating, improving efficiency.
In-Situ Resource Utilization (ISRU): Solar concentrators could use sunlight for heating and 3D printing/sintering, potentially reducing reliance on pure PV cells.
Advanced Motors/Generators: Electric motors are preferred over combustion engines due to simplicity; next-gen storage like supercapacitors could revolutionize rapid power delivery.
Considerations for a Mars Garage
Dust Mitigation: Systems to clean solar panels and protect equipment from fine dust are crucial.
Thermal Management: Dealing with extreme cold (using waste heat or electrical heaters) is vital for equipment and battery health.
Scalability: A mix of sources (solar for peak, nuclear for baseline) offers the best resilience, from small tools to large fabricators

As you can see they are not standard

#20 Re: Not So Free Chat » NASA's new leader makes his priorities clear on day one » Yesterday 14:45:51

Oldfart1939 wrote:

I am very enthusiastic with the appointment of Jared Isaacman as NASA Administrator!

Here's a link to this excellent interview!

https://www.youtube.com/watch?v=hnwyh2B … WL&index=1


Sorry that the name was not in my original title but we know this as being more politically delivered than anything else.

#21 Re: Human missions » Why Artemis is “better” than Apollo. » Yesterday 14:43:26

That's going to happen when management tries to be engineers looking at balance sheets rather than performance.
So which shield type is this one as I remember the original PICA version was dismissed for the honey combo hand inserted materials to which this one makes me wonder...

#22 Re: Human missions » Why Artemis is “better” than Apollo. » Yesterday 14:39:53

GW Johnson wrote:

The odds favor their survival,  but the lethal uncertainty is nowhere near zero.  Initially,  the excuse was eliminating the skip and just going for direct entry.  I do not see anything of that plan in the recent stories.  This reminds me eerily of Challenger and Columbia. 

I am still disappointed seeing the entire debate framed only as "fly what you have" vs "total redesign".  Total redesign is NOT required,  all they need to do is go back to the labor-intensive hand-gunned heat shield.  There is NO REDESIGN associated with that!  They already HAVE that design!  They already flew it!

Doing that would enable them to work out how to cast those tiles with the hex cores in the them,  and fly such a thing,  even as a subscale test article,  to see it actually work right.  I already showed how to do that revised processing with an extrusion press,  here on these forums,  and I already sent that idea to them via a contact I knew within NASA,  who has since retired.  I NEVER EVER heard back from their heat shield people,  to whom my contact forwarded my materials.  "Not invented here" is a real flaw shared by lots of big organizations! 

But it would definitely work,  because the fibrous nature of the charred hex helps tie the otherwise weak carbon char together.  It's a composite material that is better than just the carbon char from the polymer alone.  I know that because of my experience with ablatives in ramjets and solid rockets.  If you cannot reinforce the char,  it goes away too quickly,  in one fashion or another.  Which experience goes way beyond sample testing in an arc jet tunnel,  and running CFD codes that usually do not deserve to be believed,  without confirmation testing!  I'm talking real burn experiences with real motors and engines here!

The Artemis 1 failure already proved that fiber reinforcement contention of mine!  The only difference between Artemis 1 and the first Orion that flew was that they deleted the hex to cast the tiles instead of hand-gunning the polymer into a hex core already attached to the capsule,  like Apollo.  Which is what flew on the first Orion.  That's NOT a FULL re-design of anything,  it's only a variation on the cast tile processing they now prefer (at the risk of the crew's lives,  I might add,  if they don't do something to reinforce that char).

GW

#23 Re: Meta New Mars » Housekeeping » Yesterday 13:16:38

off topic solving of potential failures within a project is just what the fishbone is for..

Fishbone theory, or the Fishbone Diagram (also known as an Ishikawa Diagram or Cause-and-Effect Diagram), is a visual tool for root cause analysis that maps out potential causes of a problem in a fish-skeleton-like structure, helping teams brainstorm, categorize, and identify underlying issues, not just symptoms, for better problem-solving in quality control and management. The problem is the "head," and major causes branch off the "backbone" as "ribs," with sub-causes extending further, revealing hidden linkages and process bottlenecks for future improvements.

you have you own topic of import everything to do you process within to make the garage that you want on mars.

I have already shown that import everything on the first connex box transport is not sustainable as the equipment gets larger to perform the task of building increases.

#24 Re: Human missions » Why Artemis is “better” than Apollo. » Yesterday 11:12:32

tahanson43206 wrote:

For GW Johnson...

https://www.msn.com/en-us/news/technolo … e130a&ei=8

I think this is the best way to preserve items that would disappear over time.

The story at the link above reports on a personal review of the heat shield for Artemis II by the new NASA director.

(th)

NASA chief puts Orion heat shield through final go/no-go check

AA1TZpdf.img?w=768&h=432&m=6

On the eve of the first crewed flight of the Artemis program, NASA’s top leadership has zeroed in on a single, unforgiving piece of hardware: the Orion capsule’s heat shield. The final go or no-go review of that system is not just a technical milestone, it is a public test of whether the agency has truly learned from the scorching lessons of Artemis I and is ready to send astronauts back toward the Moon.

By personally scrutinizing the Orion heat shield before Artemis II, the new NASA chief is signaling that the agency’s confidence must be earned, not assumed. The outcome of that review will shape when the mission flies, how the crew returns, and how the public judges NASA’s willingness to confront uncomfortable risks in full view.

From char loss mystery to root cause
The scrutiny now focused on Orion’s heat shield began the moment the uncrewed Artemis I capsule was pulled from the Pacific and hauled back to shore. After NASA recovered the Orion spacecraft and transported it to NASA’s Kennedy Space Center, engineers found that parts of the charred layer on the ablative shield had come off in ways they did not fully predict, a surprise for a system designed to burn away in a controlled fashion during reentry. That discovery triggered a long investigation into why chunks of material were shedding, and whether the pattern hinted at a deeper design flaw in the thermal protection system that guards the crew module.

Investigators eventually traced the problem to how the material behaved under the specific heating and airflow conditions of the Artemis I trajectory, rather than to a single manufacturing defect or obvious structural crack. NASA has described how the charred layer on Orion’s base heat shield experienced unexpected char loss, prompting teams to dissect the shield, model the aerothermal environment, and compare test data with flight telemetry. That work set the stage for the current go or no-go decision, because it forced NASA to decide whether the anomaly could be bounded with analysis and minor tweaks, or whether a more invasive redesign was needed before putting people on board.

Why Artemis II depends on a single shield
The stakes of that decision are clear when I look at what Artemis II is supposed to do. The mission will send a crew of four, including Christina Koch, on a loop around the Moon and back to Earth, exposing Orion to a high-speed reentry that is only slightly less punishing than a direct lunar return. Koch and the other members of the Artemis 2 crew are eager to launch on their mission, but their path home runs straight through the same thermal environment that stripped away char on Artemis I, and any uncertainty about the shield’s performance becomes a direct question about crew safety.

NASA has already acknowledged that the next flight is a crucial stepping stone toward a sustained lunar presence and, eventually, the kind of deep-space expeditions needed for crewed Mars missions. The agency’s decision to proceed with Artemis II using the existing Orion heat shield design, rather than ripping it out, followed an extensive review of the Artemis I data and a formal update to the broader Artemis flight plan. That choice effectively ties the schedule for returning humans to lunar orbit to the confidence engineers and leadership can place in a single, upgraded but not fundamentally redesigned shield.

Skip entry, schedule pressure, and a narrow launch window
The technical debate around Orion’s protection system is inseparable from the way the capsule comes home. For Artemis I, NASA used a “skip entry” profile in which Orion dipped into the atmosphere, then briefly bounced back out before making its final descent, a maneuver that spreads heating over a longer path but also creates complex aerodynamic loads. NASA traced the problem in part to Orion’s skip entry trajectory, noting that the pattern of char loss matched the phases when the capsule was skimming the upper atmosphere and then diving back in, which is why the same profile for Artemis II has drawn so much attention from engineers and outside analysts alike.

All of this is unfolding against a tight but flexible launch window that could open as soon as early February. NASA’s Artemis II mission is currently targeted to launch in February, with officials describing a window that stretches from Feb. 6 to April 10 and is broken into several distinct periods of possible liftoff opportunities. Local coverage has underscored how the mission, updated at 10:24 PM EST, will be the first time astronauts fly around the Moon since Apollo, and that schedule pressure is now colliding with the need to be absolutely certain about the heat shield’s behavior on another skip entry.

nside the new NASA chief’s go/no-go moment
Into this mix has stepped a new NASA administrator, Jared Isaacman, who has made a point of personally engaging with the Orion heat shield issue. In a detailed review session described by space reporter Eric Berger, Isaacman pressed engineers on what went wrong with Artemis I and what had changed for Artemis II, before ultimately expressing full confidence in the system. That level of openness and transparency is exactly what should be expected of NASA, Berger wrote, noting that Isaacman had only been sworn in on December 18 when he convened the review that would effectively serve as the final go or no-go check for the shield, a moment captured in Jan coverage of the meeting.

What stands out to me is how candid the internal conversation appears to have been. According to a detailed account shared by one attendee, the NASA team spent most of the session walking through charts and models before, toward the end of the meeting, agreeing to discuss something that no one really liked to talk about: the residual risk that cannot be engineered away. One of the NASA engineers said that even with all the analysis, there is still a nonzero chance of unexpected char behavior, a comment that surfaced in a However detailed community write-up of the review. Isaacman’s decision to accept that residual risk, while insisting on continued testing and monitoring, is the essence of a go call in human spaceflight.

Rollout, wet dress, and what still worries engineers
Even as the heat shield debate plays out in conference rooms, the hardware for Artemis II is moving toward the pad. NASA plans to roll out the Space Launch System rocket for the mission on Jan. 17, a key step that will lead into a full “wet dress rehearsal” where teams load the core stage and upper stage with more than 700,000 g of cryogenic propellants, roughly 2.65 m liters, and run through the countdown. During wet dress, teams demonstrate the ability to load more than 700,000 g of supercold fuel without leaks or valve issues, a rehearsal that must succeed before anyone worries about the heat shield’s performance on the way home.

Behind the scenes, though, some specialists remain uneasy about how much of the Artemis I anomaly has been retired by analysis alone. A detailed video breakdown posted in Jan by an independent analyst revisited the Orion heat shield investigation and walked through what char loss really means for the structure underneath, highlighting how localized material shedding could, in a worst case, expose underlying layers to higher heating than expected. That follow-up on Orion underscored that while NASA’s official line is that the shield is safe for flight, there is still a healthy debate in the technical community about whether the current design has enough margin for the long-term Artemis roadmap.

Delay debates, outside critics, and the politics of risk
The path to this moment has already included one major schedule reset. In Dec, NASA announced that it would delay the next flight of the Aremis program, Artemis 2, pushing the mission back from its earlier target so engineers could fully understand the heat shield behavior and other systems. That decision, dissected in a widely viewed explainer on why NASA is not fixing the heat shield on Artemis II, made clear that the agency preferred to accept a longer gap between flights rather than rush a redesign that might introduce new unknowns, a tradeoff that was laid out in detail in a NASA-focused analysis of the delay.

Critics have also questioned whether the nomination of Jared Isaacman, a billionaire pilot with his own commercial spaceflight ambitions, has overshadowed the technical issues around Orion. In Dec, one commentator argued that the Isaacman nomination risked pulling attention away from the hard engineering questions and toward personality-driven coverage, urging viewers on Thursday to focus instead on the new information about the heat shield and its test history. That perspective, shared in a detailed Thursday breakdown of the nomination, reflects a broader tension: NASA must balance the political optics of bold leadership with the unglamorous work of resolving char patterns and thermal margins.

Crew confidence and the long road back to the Moon
For the astronauts assigned to Artemis II, the heat shield debate is not an abstract engineering exercise. Christina Koch has spoken about how she and her crewmates are preparing for a mission that will test not only Orion’s systems but also the procedures and teamwork needed for later landings, and Koch and the other members of the Artemis 2 crew are eager to launch on their mission as soon as NASA gives the final green light. Their confidence rests on the assurance that the same shield which protected an uncrewed capsule through a skip entry will do the same with four people strapped inside, a point underscored in a feature on how Koch and the crew are training for the unknowns they might encounter around the Moon.

NASA’s own messaging has tried to thread the needle between caution and ambition. Agency leaders have emphasized that the Artemis architecture, including Orion’s heat shield, is being built not just for a single lunar flyby but for a series of increasingly complex missions that will eventually support long-duration stays on the surface and, further out, crewed Mars expeditions. Local television coverage in Jan, updated by reporter Meghan Moriarty and reporter Hayley Crombleholme, has highlighted how the Artemis II mission to launch in February is framed as a historic return to deep space that must still clear a rigorous safety bar before liftoff. That framing, captured in a Meghan Moriarty segment, shows how the final go or no-go on the heat shield has become a proxy for the public’s trust in NASA’s entire lunar strategy.

What the final call will really decide
As the rollout date approaches, the agency is also refining its launch opportunities and contingency plans. NASA has broken the Artemis 2 launch window into three periods, each with a restricted set of possible liftoff times that balance lighting conditions, communications coverage, and the geometry of the return corridor. That structure, outlined in a Jan update on how Artemis 2 will move to the pad and aim for dates between Feb. 6 and April 10, underscores how tightly the mission’s trajectory, including the skip entry, is woven into the calendar.

In parallel, public-facing explainers have reminded viewers that the heat shield will face its biggest test yet when Orion comes back from the Moon with people on board. One recent overview noted that the same skip entry profile that contributed to char loss on Artemis I will again be used to manage g-forces and heating, and that NASA traced the earlier problem in part to that trajectory while still concluding the system is safe for flight. That assessment, summarized in a Jan report on the upcoming mission, makes clear that the final go or no-go check by the NASA chief is less about discovering a new flaw and more about affirming that the agency is willing to own the residual risk it has already mapped.

#25 Re: Life support systems » Power generation on Mars » Yesterday 10:48:23

tahanson43206 wrote:

For SpaceNut re electrical fittings in the garage on Mars.

A solution is to decide upon a single electrical system for Mars.

This would require negotiation before any Nation lands on Mars.

We have international standards for many aspects of modern society.

Setting up standards for Mars seems possible before the kind of mess you've described occurs.

In the mean time, you have the power to simply declare what fixtures your be, and continue with your garage plan.

(th)

Another fishbone topic of power

And yet with standards we still power things with different battery voltages, transmit AC power in 50 and 60 cycles, Single phase AC with ranges, Multi phase is a number of phase angle relationships, high voltage DV and AC transmission lines, ect.. Mars will use all as we do here.

This brings up the next fishbone topic Power Distribution by pipelines on Mars.

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