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The Space Shuttle That Never Flew: Lockheed’s LS-200
n 1966, the United States Air Force and Lockheed introduced the Star Clipper concept. At the time, it was “an Earth-to-orbit spaceplane based on a large lifting body spacecraft and a wrap-around drop tank.”
After 1966, NASA began a space program that included a permanently manned space station, a small base on the moon, and the hopes of a soon-to-be crewed mission to Mars. This is where the concept of a “logistics vehicle” emerged in order to lower the cost of space station operations. The vehicle’s role would be focused on changing crews on the space station on a weekly basis.
In 1967, a whole-day meeting was arranged to evaluate the logistics vehicle concept. The Air Force and NASA had already joined forces on a study of existing technologies in the “Integrated Launch and Re-entry Vehicle” project, or ILRV. The meeting resurfaced the ILRV research calling on the same industry partners to present different logistics vehicle concepts.
That’s when Lockheed submitted Star Clipper while General Dynamics introduced their Triamese and Chrysler SERV. Soon, NASA’s own teams joined in on the fun supporting mostly the “classic” flyback design.
Then in 1971 something happened that changed everything and brought the Star Clipper to the forefront. The maximum development budget was reduced by 50% by the Office of Management and Budget, going from a whopping $10 billion to a mere $5 billion.
This is when the Star Clipper became the most viable option as the costs for a stage-and-a-half design were much lesser because it involved the engineering of only one spacecraft. Despite this, in the end, it was not Lockheed’s version that would eventually be chosen to be built, but North American Aviation’s take on the concept.
almost sounds like they are just butting the tiles edges to each other rather than using a gap filler material.
it could also be made to drive pistons for air compressing as well.
todays post show in images how its not a single layer of materials in use.
I am reminded of those old westerns that I saw as a kid with the praire covered with them.
A western water pump windmill is a device powered by wind to draw water from a well and pump it to the surface, typically used on farms and ranches in the American West to provide water for homes, livestock, and crops. Key features include a tower, a rotatable tail for facing the wind, a self-governing mechanism to adjust sail area in high winds, and a pump rod connecting to a piston in a cylinder at the bottom of the well. Daniel Halladay's 1854 invention was the first commercially successful American model, revolutionizing settlement of the Plains by making water independence possible.
How it Works
1. Wind Capture:
The wind spins the mill's blades, which are designed to catch the wind and rotate the mechanism.
2. Self-Regulation:
A tail vane turns the mill into the wind. In strong winds, the mechanism automatically turns the blades partially out of the wind to prevent damage.
3. Pump Operation:
The rotational energy is transferred down the tower by a connecting rod to a pump.
4. Water Lift:
A piston on the end of this rod moves up and down, drawing water from the well to a storage tank or another location.
Historical Significance
Settlement:
Water pump windmills made settlement on the Great Plains and other parts of the West possible by providing a reliable, independent water source.
Agricultural Expansion:
They allowed farmers and ranchers to expand operations by watering large numbers of livestock and irrigating crops without being tied to natural water sources.
Iconic Status:
Windmills became a symbol of the American West, reflecting the ingenuity and hard work of homesteaders.
Key Innovations
Daniel Halladay (1854):
.
Invented the American-type windmill, which was smaller, cheaper, and self-governing, making it practical for settlers.
Materials:
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Early models were primarily wood, but later versions incorporated metal blades and components, leading to increased durability and use.
Self-Governing Mechanism:
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This feature allowed the windmill to function reliably in a wide range of wind speeds by automatically adjusting the sail's angle or size
The current SpaceX Starship and Super Heavy booster have a stainless steel hull thickness of approximately 3.97 mm (0.156 in), and are constructed by welding together rings of stainless steel. This design marked a major shift from early carbon composite concepts for the rocket, which was originally known as the Big Falcon Rocket (BFR).
History of the Starship/BFR design
Initial carbon composite design: In 2018, early concepts for the BFR were built using carbon composites. At the time, early prototype sections were estimated to be between 12 and 25 mm thick.
Switch to stainless steel: Later in 2018, SpaceX announced the switch from carbon composites to stainless steel for the entire Starship and Super Heavy structure. Elon Musk cited reasons including lower cost, increased strength at cryogenic temperatures, and the ability of stainless steel to handle high temperatures.
First stainless steel prototypes: The first stainless steel prototypes used 301L stainless steel. Following pressure tests and iterative improvements, the alloy was updated to 304L stainless steel.
Evolution of hull thickness: The earliest steel prototypes, such as Starship SN1, were built with a 3.97 mm thickness. An anecdote from Elon Musk's biography describes his decision to push for thinner 4 mm tank walls over the nervous objections of engineers. Later, test articles like SN7.2 were briefly experimented with even thinner 3 mm steel, but recent production vehicles have remained at the 4 mm thickness.
Construction and thermal protection
Construction process: The 9-meter diameter hull is manufactured by rolling sheets of stainless steel into rings, which are then stacked and welded together.
Integrated structure: The stainless steel hull acts as both the external skin and the propellant tanks for the vehicle's liquid methane and liquid oxygen.
Heat shield for re-entry: While the steel can withstand high temperatures, the side of the Starship that faces the wind during re-entry is covered with approximately 18,000 hexagonal ceramic tiles for additional thermal protection.
Continuous development: SpaceX continues to iterate on the design and materials used. Following flight test 4, upgraded heat shield tiles were installed on the flight 5 Starship, along with a secondary ablative layer underneath the tiles for added protection against overheating
It appears that the tank wall and hull walls are each of the same thickness to which the sregnth comes from the connecting area of both as it rises from the ground skyward.
The current SpaceX Starship and Super Heavy booster have a stainless steel hull thickness of approximately 3.97 mm (0.156 in), and are constructed by welding together rings of stainless steel. This design marked a major shift from early carbon composite concepts for the rocket, which was originally known as the Big Falcon Rocket (BFR).
History of the Starship/BFR design
Initial carbon composite design: In 2018, early concepts for the BFR were built using carbon composites. At the time, early prototype sections were estimated to be between 12 and 25 mm thick.
Switch to stainless steel: Later in 2018, SpaceX announced the switch from carbon composites to stainless steel for the entire Starship and Super Heavy structure. Elon Musk cited reasons including lower cost, increased strength at cryogenic temperatures, and the ability of stainless steel to handle high temperatures.
First stainless steel prototypes: The first stainless steel prototypes used 301L stainless steel. Following pressure tests and iterative improvements, the alloy was updated to 304L stainless steel.
Evolution of hull thickness: The earliest steel prototypes, such as Starship SN1, were built with a 3.97 mm thickness. An anecdote from Elon Musk's biography describes his decision to push for thinner 4 mm tank walls over the nervous objections of engineers. Later, test articles like SN7.2 were briefly experimented with even thinner 3 mm steel, but recent production vehicles have remained at the 4 mm thickness.
Construction and thermal protection
Construction process: The 9-meter diameter hull is manufactured by rolling sheets of stainless steel into rings, which are then stacked and welded together.
Integrated structure: The stainless steel hull acts as both the external skin and the propellant tanks for the vehicle's liquid methane and liquid oxygen.
Heat shield for re-entry: While the steel can withstand high temperatures, the side of the Starship that faces the wind during re-entry is covered with approximately 18,000 hexagonal ceramic tiles for additional thermal protection.
Continuous development: SpaceX continues to iterate on the design and materials used. Following flight test 4, upgraded heat shield tiles were installed on the flight 5 Starship, along with a secondary ablative layer underneath the tiles for added protection against overheating
Each stage also has seperate 100mT fuel for return to earth landing in header tanks.
o build the fuel tank and structure of Starship, SpaceX manufactures stainless steel rings, assembles them into larger sections with domes, and stacks these sections vertically. Advanced robotic welding, internal stiffeners, and a common bulkhead are key to integrating the tank's pressure vessel with the overall vehicle structure.
Manufacturing steel components
Steel coils: The process begins with delivery of 11-ton coils of 3.97 mm (0.156 in) thick stainless steel to the Starbase production facility.
Forming rings: Robotic machinery unrolls and forms the steel into 9-meter diameter circles, then welds them into continuous rings that are 1.83 meters (6 ft) tall.
Fabricating domes: Tank domes, which act as the top and bottom caps of the tanks, are made from stamped and welded steel panels. This includes the crucial common bulkhead that separates the liquid oxygen (LOX) and liquid methane (CH4) tanks.
Welding and assembly
Robotic welding: SpaceX uses advanced robotic welding techniques, including laser, electron beam, and friction-stir welding, to join the steel sections. This ensures high-precision, stronger welds compared to earlier manual welding.
Section stacking: Individual rings are stacked and welded into larger barrel sections. Domes are integrated into these sections, often on the ground, before final vertical stacking.
Vehicle stacking: A Starship's assembly progresses from the top down. Sections like the nosecone and header tanks are added to the common dome section, which is then joined to the main tank and engine sections.
Integrating structural integrity
Internal stiffeners: Internal stringers (axial reinforcements) and baffles are welded inside the tanks. This improves the vehicle's structural rigidity, prevents the propellant from sloshing, and allows the structure to support its own weight without internal pressure.
Common bulkhead: A highly optimized, mass-saving common bulkhead serves as the top of the LOX tank and the bottom of the CH4 tank, eliminating the need for a separate tank wall between them.
Engine thrust structure: The aft dome of the LOX tank is integrated with a heavily reinforced thrust puck. This specialized structure transfers the immense thrust from the Raptor engines directly into the vehicle's frame during flight.
Testing and completion
Proof testing: After the structure is assembled, it undergoes cryogenic proof testing, where it is filled with liquid nitrogen and pressurized beyond flight levels. This confirms the vehicle's structural integrity at cryogenic temperatures.
Engine installation: Following successful testing, the Raptor engines are installed, along with plumbing, avionics, and flight-control surfaces like the flaps.
Thermal protection system: The heat shield tiles are then attached to the exterior of the vehicle to protect it during atmospheric re-entry
https://www.teslarati.com/spacex-starsh … rage-tank/
Fuel tank as part of structure
https://newmars.com/forums/admin_bans.php
enter * in the username box and hit submit to get the list
these are the banned users but they are not a group, each user is removed from the banned table only 1 at a time.
https://newmars.com/forums/admin_users.php
enter * in the username box and hit submit to get the list
this shows the Title/Statuss and those are inactive, members ect including the banned identies.
you can change the group to inactive but it is still a banned user if not removed from the individual under the first list.
The users m* that were change have not had info changed for the profile. I think we would still want to change the username and default the email to keep it locked out in the profile.
How much food and water do you need for a one-year stay on Mars?
Nutritionists recommend that you drink at least eight 8-ounce glasses of water a day. Let's say you might be a tad thirstier. So for a two-year mission, a person would need about 456 gallons (1,726 liters) of water.
If you want to be a minimalist about it, you can get your calories from white sugar, your fat from vegetable oil, your protein from protein powder and your fiber from bran. In this case, each person on the two-year journey would need:
602 pounds (274 kilograms) of sugar
133 pounds (60 kilograms) of vegetable oil
96 pounds (43 kilograms) of protein
40 pounds (18 kilograms) of fiber
If you formed all of those ingredients into bars or kibble, you would need about 880 pounds, or 400 kilograms, of food per person. When you buy dog food at the grocery store, a typical large bag holds 20 pounds (9 kilograms). So you would need 44 large dog-food-sized bags to keep one person alive for two years.
Bad example but the point is we are going to need to solve it for 3 different legs and staging of what we need.
https://en.wikipedia.org/wiki/Space_food
https://ift.onlinelibrary.wiley.com/doi … 10.01982.x
The different forms in which food is provided include the following:
1
Thermostabilized—this process, also known as the retort process, heats food to a temperature that renders it free of pathogens, spoilage microorganisms, and enzyme activity. NASA thermostabilized products include pouched soups, sides, desserts, puddings, and entrees.2
Irradiated—irradiation is not typically used to process foods to commercial sterility. However, NASA has received special dispensation from the Food and Drug Administration (FDA) to prepare 9 irradiated meat items to commercial sterility (FDA 2009).3
Rehydratable—both commercial and internally processed freeze-dried foods are included in the NASA food provisions and then rehydrated during the mission using the potable water supply. Rehydratable foods are typically side dishes, such as spicy green beans and cornbread dressing, or cereals. Ambient and hot water are available to the crew for rehydration of these items.4
Natural form—natural form foods are commercially available, shelf stable foods. The moisture of the foods may range from low moisture (such as almonds and peanuts) to intermediate moisture (such as brownies and dried fruit), but all have reduced water activity, thus inhibiting microbial growth. These foods help to round out the menu by providing very familiar menu options, additional menu variety, and foods requiring no preparation time.5
Extended shelf life bread products—items, such as scones, waffles, tortillas, and dinner rolls, can be formulated and packaged to give them a shelf life of up to 18 mo. Like the natural form foods, breads add to menu variety and address crewmembers’ desire for familiarity.6
Fresh food—foods such as fresh fruits and vegetables, which have a short shelf life, are provided on a limited basis, more for psychological support than as a means to meet dietary requirements.7
Beverages—the beverages currently used on the International Space Station (ISS) and the Space Shuttle are either freeze-dried beverage mixes (such as coffee or tea) or flavored drinks (such as lemonade or orange drink). The drink mixes are weighed and then vacuum sealed inside a beverage pouch. In the case of coffee or tea, sugar or powdered cream can be added to the pouch before sealing. Empty beverage pouches are also provided for drinking water.
Only 13 pages but full of information
Human Mars Mission Design – The Ultimate Systems Challenge
Mars Landing Vehicles: Descent and Ascent Propulsion Design Issues
AI Overview
For a two-manned Mars mission, food and supplies must cover a multi-year journey, including six months of transit each way and a long stay on the surface. Astronauts would rely on a hybrid system: a supply of packaged, shelf-stable food and advanced regenerative systems for producing fresh food, recycling water, and managing waste.Food system
The food system must be nutritious, reliable, and varied to prevent "menu fatigue," which can lead to inadequate calorie intake.
During transit (approx. 6 months each way)
Packaged meals: The crew would rely on food similar to that on the International Space Station (ISS), but with a shelf life of three to five years. Examples of current space foods include thermostabilized pouches, rehydratable meals, and intermediate-moisture items like nuts and crackers.Menu variety:
Menus are typically on a weekly rotation to provide variety and psychological comfort. Food scientists at NASA's Space Food Systems Laboratory develop and test space foods for nutritional value, taste, and safety.
Nutritional supplements: Vitamins and minerals, particularly Vitamin D, Vitamin K, and calcium, are crucial for mitigating bone and muscle loss in microgravity.Low-sodium food:
To prevent excessive calcium excretion, a negative effect of high sodium intake, space food is being reformulated to reduce sodium content.On Mars' surface (approx. 18 months)
In-situ food production:
Crew members would grow crops in a specialized habitat to supplement pre-packaged meals. This provides fresh produce, reduces reliance on Earth, and offers psychological benefits.Potential crops:
NASA's analog missions test crops like leafy greens, herbs, and small fruits. The European Space Agency (ESA) has also researched staple crops such as potatoes, wheat, and soybeans.Food processing:
A Martian galley would allow astronauts to process and cook the harvested ingredients.Waste management:
Used food packaging must be efficiently managed since there is no way to incinerate it. Lighter materials with sufficient barrier properties will be used.Supplies and equipment
In addition to food, a Mars mission requires highly reliable and efficient life support systems, medical gear, and crew equipment.
Life support and environmental controlWater recycling systems:
Closed-loop systems are essential for recycling water from urine, wastewater, and humidity. Water can also be extracted from Martian soil and ice.Atmosphere revitalization:
Regenerative systems would scrub carbon dioxide (CO2) from the air and use it to produce oxygen (O2). Crop growth would also contribute to oxygen production.Radiation shielding:
Specialized gear or materials are needed to protect the crew from high radiation exposure during transit and on the Martian surface.Temperature control:
Reliable systems for managing temperature and humidity inside the habitat.Health and hygiene
Medical kit:
A lightweight, compact, but comprehensive medical kit is necessary. Researchers use predictive models to determine the most likely health issues and prioritize supplies.Exercise equipment:
Compact exercise gear, such as resistance bands, is vital for combating muscle atrophy and bone loss in a low-gravity environment.Personal hygiene:
Toothbrushes, wet wipes, and sanitizer. Water-conserving systems are essential for laundry and personal cleaning.Mission and surface exploration
Spacesuits:
Extravehicular Activity (EVA) suits are required for surface exploration and emergencies.Power systems:
Reliable and lightweight power sources, such as fission surface power systems, are needed to power all equipment.
Communication: Equipment for constant communication and navigation.Scientific equipment:
Tools and instruments for research and exploration
The colors of the starship reminds me of the wind tunnel testing Nasa would do on a model. So this method is pretty ugly.
its why going with a large heat shield diameter for mars is favored for getting more to the surface of mars as mass also plays into the equation.
Starting to get wild and crazy.
Gulf on alert for hurricanes during 2nd half of September
Based on recent SpaceX flights, the white residue on Starship's nose cone after reentry is from ablative insulation material that became exposed to the high heat of atmospheric entry. This occurred in areas where SpaceX deliberately removed some of the protective tiles for testing.
For example, after a late August 2025 flight, SpaceX CEO Elon Musk confirmed that the discoloration was the result of a thermal protection system experiment.
The purpose of the experiment
Testing different heat shield designs: SpaceX has been experimenting with various thermal protection configurations. On recent flights, the company has intentionally removed some of Starship's heat shield tiles to test different materials, including metallic tiles, and to see if other systems can compensate for missing tiles.
Exposing the insulation: In the areas where the tiles were removed, the underlying white ablative insulation was directly exposed to the high-temperature plasma of reentry.
Creating a white vapor deposit: The extreme heat caused some of this insulation material to vaporize. This vapor then re-condensed as a white coating on the cooler sections of the nose cone.
A different kind of test
The ablative insulation that appeared white after reentry is a departure from the polished steel Starship prototypes. For certain operational versions, like the Human Landing System (HLS) for the moon, a white thermal coat will be used. This is done to reflect sunlight and help with temperature regulation while in space. However, the post-reentry white residue is a byproduct of a specific experimental process, not the intended final coloration
AI Overview
Starship turned orange after re-entry due to experimental metallic heat shield tiles that oxidized, forming iron oxide. This orange color is a result of these metallic test tiles reacting with atomic oxygen in the atmosphere at high speeds, while white patches were from deliberately removed tiles exposing white insulation. This discoloration indicates the success of these new metallic tiles and insulation testing during Flight 10, with Elon Musk confirming the phenomenon was intended to observe these materials.
Details of the Orange Coloration
Metallic Test Tiles:
The primary cause of the orange coloration was the use of experimental metallic heat shield tiles on the flight.
Oxidation:
These metallic tiles, likely stainless steel, oxidized rapidly during re-entry at Mach 25, reacting with the atmospheric oxygen to form a distinct orange, iron oxide layer.
Intended Experiment:
SpaceX deliberately placed these metallic tiles in specific areas and intentionally removed some ceramic tiles to expose the underlying insulation.
White Areas and Insulation
Deliberate Removal:
The white areas seen on Starship are from areas where the standard ceramic heat shield tiles were intentionally removed to test the white insulation beneath.
White Insulation:
This insulation, made of heat-resistant composites, was designed to withstand re-entry temperatures and reflect heat. Unlike the metallic tiles, it did not contain easily oxidizable metals, causing it to retain its white color.
Significance of the Event
Testing and Reusability:
The orange discoloration is not a sign of failure; rather, it's a visual indication of SpaceX's ongoing material science experiments to develop and test new thermal protection systems for future Starship missions, aiming for increased reusability.
Confirmation of Success:
Elon Musk confirmed that the heat shield tiles largely stayed attached, suggesting the latest upgrades are performing well, despite the unusual colors.
AI Overview
The Bestagons: Starship's Upgraded Heat Shield
Starship currently uses black, hexagonal ceramic heat shield tiles, likely a derivative of the TUFROC material, mounted on a stainless steel hull, to protect it from re-entry temperatures. For the future, SpaceX is exploring a metallic heat shield technology that utilizes the spacecraft's liquid methane to perform film cooling.Current Ceramic Tiles
Composition: The tiles are made of a toughened, porous, fibrous ceramic material, possibly a version of the TUFROC (Toughened Unipiece Fibrous Reusable Oxidation-Resistant Ceramic) used on other spacecraft.
Color: They are black to help radiate heat away from the vehicle more quickly.
Structure: The tiles are mounted directly onto Starship's stainless steel body.
Function: They are designed to withstand the extreme temperatures of atmospheric re-entry and can be reused for multiple missions.
Future Metallic Heat Shield
Concept:
SpaceX is developing and experimenting with a metallic heat shield system.
Mechanism:
This system incorporates tiny holes in the metallic plates. During re-entry, the liquid fuel (water or methane) seeps through these holes, creating a film that carries away heat and prevents the underlying metal from melting.
Advantages:
Metallic shields offer greater durability, are easier to manufacture in larger sections, and are simpler to repair or replace than ceramic tiles.
Material:
While experimental, the material used for this project is expected to be a heat-resistant alloy or stainless steel.
AI Overview
Starship SN9's Heatshield : r/SpaceXLounge
Starship's metal tiles are composed of SpaceX's proprietary "30X" stainless steel alloy, an evolution from commercially available 301 and 304L grades, featuring custom refinements with potentially higher chromium content for improved corrosion resistance and strength. This proprietary alloy was developed in-house to overcome limitations of previous materials, and while its exact composition is undisclosed, it is an austenitic stainless steel tailored for the extreme conditions of spaceflight.Evolution of Starship's Materials
Early stages:
Initially, Starship used commercially available stainless steel alloys, such as 301 and 304L.
Transition to proprietary alloy:
SpaceX eventually transitioned to a custom alloy, internally designated "30X," for the vehicle's construction.
Current material:
The current standard for Starship and the Super Heavy booster is this proprietary stainless steel.
Characteristics of the "30X" Alloy
Proprietary development: The "30X" alloy is a custom formulation developed by SpaceX.
Enhanced performance: It incorporates custom refinements and potentially higher chromium content than standard grades, leading to increased resistance to corrosion and degradation.
High-strength properties: The material is an austenitic stainless steel designed to withstand the harsh conditions of space launch and re-entry.
Why Stainless Steel for Starship?
Cost-effectiveness:
Stainless steel is relatively inexpensive compared to other high-strength materials like titanium.
Machinability:
It is easier to machine and work with, which is crucial for constructing large structures like Starship.
Cryogenic strength:
Stainless steel maintains its strength at cryogenic temperatures, essential for spaceflight operations.
Resilience:
The alloy's ability to form a protective oxide layer prevents corrosion and degradation, even after multiple missions
The tile material sure did not standup to the entry but a shuttle tile system would require lots more prep time. The transpiring would mean thicker metals to widthstand the boiling pressure between the layers that would hold the water or other working fluids.
We have talked about this in
Starship is Go... Human missions
Landing on Mars Human missions
VentureStar is it possible now Interplanetary transportation
transpiring heat shield pressure on entrry
When a spacecraft with a transpiring heat shield reenters the atmosphere, pressure is used to force a coolant through a porous surface. The coolant absorbs heat and forms a protective gas layer, which creates its own internal pressure that interacts with the high-pressure shockwave from the atmosphere to protect the vehicle.
Mechanism of transpiration cooling
High-pressure coolant injection: A pressurized coolant, such as a gas or liquid, is stored inside the vehicle. For reentry, a gas like Argon is often used. This coolant is forced through thousands of small pores or channels in the heat shield's surface.
Heat absorption: As the coolant travels through the porous wall, it absorbs a portion of the vehicle's internal heat via convection. If the coolant is a liquid, it also absorbs a large amount of heat during its phase change into a gas (evaporative cooling).
Boundary layer interaction: Upon exiting the pores, the cold coolant gas creates a protective film or cushion between the heat shield's surface and the superheated atmospheric gas. This "thermal blowing effect" reduces heat transfer from the extremely hot boundary layer to the vehicle.
Pressure coupling: The high-pressure injection of the coolant into the boundary layer pushes the hot atmospheric gas away from the surface. This creates a pressure gradient that helps to keep the cold gas layer stable and prevents the hot, turbulent air from reaching the surface.
Managing pressure on entry
The immense pressure on a spacecraft during atmospheric reentry is caused by rapidly compressing the air ahead of it. A transpiring heat shield manages this pressure in several ways:
Balancing internal and external pressure: To ensure proper functioning, the internal pressure used to push the coolant out must be sufficient to overcome the external stagnation pressure of the air rushing past the vehicle. Advanced systems can couple the coolant injection velocity to the wall pressure to maintain optimal performance.
Preventing turbulence: If the internal pressure is too high, the injected coolant can cause the boundary layer to transition from a stable laminar flow to a more chaotic and destructive turbulent flow. This can decrease the heat shield's effectiveness and even increase heat transfer in some cases.
Adapting to conditions: The transpiration cooling system must be actively controlled to optimize the coolant flow rate for different speeds and altitudes during reentry. High heat load areas, such as the nose cone of a capsule, may require more coolant injection than others.
Advantages and disadvantages
Transpiration cooling is a promising technology for next-generation reusable spacecraft, but it has trade-offs compared to traditional heat shields.
Advantages
High reusability: Unlike ablative heat shields, which burn away on a single use, a transpiring heat shield can be used multiple times.
Active control: The system allows for dynamic adjustment of cooling based on real-time flight conditions.
Reduced mass: The protective layer of gas allows for lighter-weight protective materials compared to passive shields.
Disadvantages
Complexity: An active cooling system is more complex than a passive one, adding potential points of failure.
Vulnerability: The pores in the heat shield could become blocked, which could cause local overheating and potentially lead to catastrophic failure.
Pressure management: Balancing the internal coolant pressure against the external atmospheric pressure is a significant engineering challenge, and mistakes can lead to reduced efficiency or even greater heat loads
A "hot chimney updraft pipe" is the central component of a chimney system where an updraft, or the upward flow of hot exhaust gases, is created and maintained. This upward movement is driven by the principle that hot air is less dense than cold air, causing it to rise.
How the updraft works
The updraft is the engine of a chimney, pulling smoke and combustion gases out of a building and supplying the fire with fresh oxygen.
Temperature difference: The heat from a fire warms the air and gases inside the chimney, making them lighter than the cooler air outside. This temperature difference causes the hot, lighter air to rise.
Pressure difference: The rising hot air creates a negative pressure (low-pressure area) inside the chimney, which pulls air from the firebox and the surrounding area upward. Meanwhile, higher-pressure atmospheric air is pushed into the appliance's air intake, feeding the fire with oxygen.
Continuous cycle: This process establishes a continuous cycle of airflow that ensures smoke and dangerous carbon monoxide are vented safely outside.
Factors affecting the updraft
Several factors can influence the strength and reliability of a chimney's updraft:
Chimney height: A taller chimney generally produces a stronger updraft because it increases the pressure difference between the top and bottom of the flue. The general rule for residential systems is that the chimney pipe must be at least 3 feet above the roof and 2 feet taller than anything within 10 feet.
Temperature difference: A greater temperature difference between the inside and outside air results in a stronger draft. For example, a cold chimney can cause a reverse draft or "backdraft" when you first start a fire.
Obstructions: Blockages like soot, creosote, or debris can restrict airflow and weaken the draft.
Negative air pressure: Air-tight modern homes can create a negative pressure environment that works against the chimney's natural draft. Installing a combustion air kit or opening a window slightly can help.
Pipe configuration: Excessive bends or horizontal runs in a chimney pipe can decrease the draft, as each turn adds friction and slows the airflow.
Solving updraft issues
If a chimney isn't drafting properly, it can fill a room with smoke, which is a serious health and safety hazard. Solutions include:
Pre-heating the flue: To fix a cold backdraft, you can warm the flue with a rolled-up, lit newspaper or a heat gun for a few minutes before starting the fire. This creates a small, initial updraft to get the system working correctly.
Proper sealing: Seal any gaps or cracks around the fireplace or chimney to prevent air leaks.
Damper installation: Consider installing an air damper to better regulate airflow.
Wind considerations: A chimney cap with a special design, such as a Vacu-Stack, can prevent wind from blowing back down the chimney