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300 Liter Duda Solar Water Heater Active Split System Single Coil Tank Evacuated Vacuum Tubes Hot SRCC Certified
about $4,000 system
http://waterheatertimer.org/Pages/Famil … chart.html
A single tube
Concentrated solar evacuated tube lengths typically range from 1.5 to 2.1 meters for standard applications, with some specialized, high-temperature, or industrial models extending up to 3 meters. The length depends on the application, with typical lengths around 1.5 meters (\(~5\) feet) for residential solar hot water, while larger and more efficient systems used for industrial processes may feature longer tubes. Standard solar thermal collectors: These tubes are commonly around 1.5 to 2.1 meters in length (approx. \(~5\) to 7 feet).High-temperature and industrial applications: Some concentrated solar power (CSP) evacuated tubes designed for high temperatures can reach up to 3 meters (approx. \(~10\) feet) long.Manufacturer variations: The exact length will vary between manufacturers and specific product lines, so it is always best to check the product specifications.
While no standardized "200 gallon hot water tank power consumption chart" exists, you can calculate the approximate power consumption and use a table to present the data in BBCode. The actual figures vary based on the wattage of the unit, the temperature difference, and your household's hot water usage habits.Calculating power consumptionHere is the formula to calculate the power consumed over time:\((Power\ Consumption)\ (kWh)=\frac{Power\ Rating\ (Watts)\times Usage\ Time\ (Hours)}{1000}\)Key factorsWattage: A 200-gallon electric tank is not a typical residential size. It is a large, industrial-grade heater, and its wattage could be 10,000 watts (10 kW) or more. For comparison, large residential tanks (80 gallons) typically use about 4,500 watts.Usage time: This refers to the number of hours the heating elements are actively drawing power, not the full 24 hours in a day. It varies depending on how much hot water is used and the temperature setting.Example calculationFor the following chart, the calculation assumes a 10,000-watt (10 kW) unit with an average daily run time of 3 hours.Daily consumption: \((10\ kW\times 3\ hours)=30\ kWh\)Monthly consumption: \((30\ kWh\times 30\ days)=900\ kWh\)Yearly consumption: \((900\ kWh\times 12\ months)=10,800\ kWh\)Power consumption table (BBCode)bbcode200 Gallon Hot Water Tank - Estimated Power Consumption
(Assumes 10,000 Watt unit, 3 hours of heating per day)[table]
[tr]
[td]Time Period[/td]
[td]Approximate Power Consumption[/td]
[/tr]
[tr]
[td]Per Hour[/td]
[td]10 kWh[/td]
[/tr]
[tr]
[td]Per Day[/td]
[td]30 kWh[/td]
[/tr]
[tr]
[td]Per Month[/td]
[td]900 kWh[/td]
[/tr]
[tr]
[td]Per Year[/td]
[td]10,800 kWh[/td]
[/tr]
[/table]Note: This is an estimate. Actual power consumption depends on your unit's exact wattage, efficiency, and hot water usage
A 200-gallon electric water heater has a typical wattage of 4,000 to 6,000 watts and can consume an estimated 12 kWh per day, or 365 kWh per month, costing about \(\$36.50\) to \(\$438.00\) monthly depending on electricity rates and usage patterns. To find specific costs, use your local rate per kWh to calculate the daily, monthly, or yearly cost using the formula: \((\text{Wattage}\div 1000)\times \text{Hours\ Used}\times \text{Cost\ per\ kWh}=\text{Daily\ Cost}\). Consumption Level DailyMonthlyYearlyEstimated Wattage~4,000–6,000 watts~4,000–6,000 watts~4,000–6,000 wattsEstimated Energy Use~12 kWh~365 kWh~4,437 kWhEstimated Cost (at \(\$0.10\)/kWh)~$1.20~$36.50~$438.05Key factors affecting consumption Wattage: A larger tank generally uses more watts. Look for the specific wattage on the heater's label; a common range is 4,000 to 6,000 watts for large electric tanks.Usage hours: Water heaters are not running 24/7. A tank might cycle on for 3 to 5 hours per day.Electricity price: The cost per kilowatt-hour varies by location. Check your local utility bill for an accurate rate to get a precise cost estimate.Thermostat setting: Lowering the temperature can save energy, with a 5% to 10% reduction in energy use for every 10°F reduction in temperature.Efficiency: The model's age and insulation levels play a significant role. Newer, more energy-efficient models will consume less energy. How to calculate your specific cost Find your wattage: Check the data plate on your water heater. For a 5,000-watt heater: \((\frac{5000}{1000})=5\text{\ kW}\).Estimate daily usage: Multiply your wattage by the number of hours it runs per day, e.g., 3 hours: \(5\text{\ kW}\times 3\text{\ hours}=15\text{\ kWh}\) per day.Calculate daily cost: Multiply daily usage by your local rate. If your rate is \(\$0.15\) per kWh: \(15\text{\ kWh}\times \$0.15=\$2.25\) per day.Calculate monthly cost: Multiply the daily cost by 30: \(\$2.25\times 30=\$67.50\) per mont
AI Overview Based on your query, here is an explanation of solar thermal power for hot water, how "watts" and "watt-hours" apply, and how to represent this information using BBCode for a forum or web page. Solar thermal power for hot water Solar thermal systems heat water directly using sunlight, rather than converting it to electricity first. Because of this, the energy output is measured in heat units, not electrical units. How it works: Solar thermal collectors (flat-plate or evacuated-tube panels) on a roof absorb solar radiation to heat a fluid. This fluid then circulates through a heat exchanger to transfer the heat to a domestic hot water tank.High efficiency: Solar thermal collectors can convert up to 80% of the sun's energy into heat for water, which is a much higher conversion rate than typical photovoltaic (PV) panels. However, this is not an apples-to-apples comparison, as PV produces electricity, which can be used for a wider variety of purposes."Watts" in context: When discussing solar thermal systems, the term "watts" (\(W\)) is used to describe the instantaneous rate of heat transfer, typically expressed as thermal kilowatts (\(kW_{th}\)). A common conversion factor is \(0.7\) \(kW_{th}\) per square meter of collector area. Electrical watts (\(W\)) are only relevant for the small amount of power needed to run pumps and system controls. Calculating and expressing energy output For solar thermal, it is most accurate to measure the total energy output over time. Watt-hours (\(Wh\)): This is a unit of energy equal to the power in watts multiplied by the time in hours. For solar thermal, this would represent the total thermal energy (\(Wh_{th}\)) produced. For example, a system with a peak thermal output of 3.5 \(kW_{th}\) that runs for 5 hours would produce \(3,500\) \(W_{th}\) * \(5\) hours = \(17,500\) \(Wh_{th}\), or \(17.5\) \(kWh_{th}\) of thermal energy.Standard ratings: The Solar Rating & Certification Corporation (ICC-SRCC) provides standard ratings for collectors in both thermal kilowatt-hours per day and thousands of BTU per day. A typical system might produce 10–15 \(kWh_{th}\) per panel per day. BBCode for formatting BBCode is a simple markup language used on many web forums. Here is how to format text related to solar thermal power calculations for a forum post. Bold: Thermal Power:Italic: Energy output can vary based on conditions.List:bbcode
Panel Type: Evacuated Tube
Peak Output: 3.5 kW[sub]th[/sub]
Total Daily Energy: 17.5 kWh[sub]th[/sub] (over 5 sun-hours)
Formatted example:bbcodeMy Solar Thermal System Performance
This is an example of the output from a solar thermal system used for hot water.
Collector Type: Evacuated Tube
Gross Area: 3.5 m[sup]2[/sup]
Rated Thermal Power: ~2.5 kW[sub]th[/sub] (Standard conditions)
Typical Daily Energy Output:
Summer (High Radiation): 15-20 kWh[sub]th[/sub]
Winter (Low Radiation): 5-10 kWh[sub]th[/sub]
AI Overview To calculate the energy output of a solar thermal hot water system, use the specific heat formula to find the thermal energy needed to heat the water. Then, account for the system's efficiency and BBCode units. Step 1: Calculate the thermal energy needed Use the specific heat formula to determine the energy required to heat a specific volume of water:Energy (in Joules) = mass (m) × specific heat of water (c) × change in temperature (ΔT) Variables: Mass (m): The mass of water you need to heat. A common conversion is 1 kilogram (kg) per liter (L) of water.Specific heat of water (\(c\)): A constant value of approximately 4.186 Joules per gram per degree Celsius (\(4186\text{\ J/kg}\degree \text{C}\)).Change in temperature (\(\Delta T\)): The desired hot water temperature minus the incoming cold water temperature, in degrees Celsius. Example calculation:To find the energy (in Joules) required to heat 100 liters of water from 10°C to 55°C: Mass (m): \(100\text{\ L}\times 1\text{\ kg/L}=100\text{\ kg}\)Specific heat (\(c\)): \(4186\text{\ J/kg}\degree \text{C}\)Change in temperature (\(\Delta T\)): \(55\degree \text{C}-10\degree \text{C}=45\degree \text{C}\) Equation:Energy (J) = \(100\text{\ kg}\times 4186\text{\ J/kg}\degree \text{C}\times 45\degree \text{C}\)Energy (J) = \(18,837,000\text{\ J}\) Step 2: Convert to Watt-hours (Wh) Energy is commonly measured in kilowatt-hours (kWh) or watt-hours (Wh). There are 3.6 million Joules in a kilowatt-hour. Convert from Joules to Watt-hours:1 Watt-hour = 3600 Joules Equation:Energy (Wh) = \(18,837,000\text{\ J}\div 3600\text{\ J/Wh}\)Energy (Wh) = \(5232.5\text{\ Wh}\) Step 3: Estimate for BBCode formatting To represent this calculation in BBCode format, which is often used on forums and is a variation of HTML, you would structure the output with bolding for emphasis, and use code blocks if available for formulas. Example BBCode: Calculating Solar Thermal Power for Hot Water
1. Calculate Thermal Energy Needed
Energy (in Joules) = mass * specific heat * temperature change
- Mass: 100kg (for 100L of water)
- Specific Heat: 4186 J/kg°C
- Temperature Change: 45°C (from 10°C to 55°C)Energy (J) = 100 * 4186 * 45 = 18,837,000 J
2. Convert to Watt-hours (Wh)
1 Wh = 3600 JEnergy (Wh) = 18,837,000 / 3600 = 5232.5 Wh
Additional factors affecting output The calculation above is for the thermal energy required, not the solar panel output. To get a more realistic estimate of the solar thermal system's performance, you must also consider: System efficiency: Real-world systems lose energy. A factor should be applied to account for these losses.Irradiation: The amount of available sunshine, which varies by location, time of day, and weather.Collector area: The size of the solar collector panels directly impacts the amount of heat absorbed.Solar fraction: The percentage of the total hot water load that the solar thermal system is expected to provide. For a more comprehensive analysis, you can use specialized software or online calculators, such as the one offered by the U.S. Department of Energ
BTU (British Thermal Unit) Calculations
1 BTU=1 DEGREE FARENHEIT INCREASE IN ONE POUND OF WATER.
8.34 POUNDS IN ONE GALLON
BTU EXAMPLE:
Incoming water 50F outgoing water 120F 120 - 50 = DELTA T 70F
BTU's for 1 gallon of water is 70 (delta T) * 8.34 (pounds per gallon) = 583.8 BTU's
Flow Rate 2 Gallons per Minute
2 Gallons * 60 minutes = 120 Gallons per hour
120 Gallons * 583.8 BTU's per Gallon = 70,056 BTU's per HourSolar Constant (measured outside the earth's atmosphere by satellite) is about 1.3 kilowatts (1,366 watts) per square meter (kW/m²)
The maximum value is about 1 Kw (1,000 watts) per sq meter, measured at the earth's exposed surface, when the sun is directly overhead.Solar Insolation Maximum sun energy (irradiance) reaching the surface of the earth over a given time period.
kWh (kiloWatt hour) to BTU examples:
1 kWh = 3,412 btu's (per square meter when the sun is directly overhead)
90,000 btu's x 0.00029307108 = 26.37 kWhCorrect Flow Rates for Evacuated Tube Collector
0.026 to 0.066 Gallons per Minute per Tube
0.1 to 0.25 Liters per Minute per TubeVolume Equivalents
231 CUBIC INCHES PER GALLON
7.481 GALLONS PER CUBIC FOOT
1.02 GALLONS PER 100' OF ½" PIPE
2.29 GALLONS PER 100' OF ¾" PIPE
4.08 GALLONS PER 100' OF 1" PIPE
Energy Conversions
1 kWh (kilo watt hours) = 3412.1415 BTU's
1 BTU = 0.00029307108 kWh
Btu Content of Common Energy Units
1 barrel (42 gallons) of crude oil = 5,800,000 Btu
1 gallon of gasoline = 124,000 Btu (based on U.S. consumption, 2008)
1 gallon of diesel fuel = 139,000 Btu
1 gallon of heating oil = 139,000 Btu
1 barrel of residual fuel oil = 6,287,000 Btu
1 cubic foot of natural gas = 1,028 Btu (based on U.S. consumption, 2008)
1 gallon of propane = 91,000 Btu
1 short ton of coal = 19,988,000 Btu (based on U.S. consumption, 2008)
1 kilowatthour of electricity = 3,412 Btu
FormulasDELTA T = TEMPERATURE DIFFERENCE BETWEEN TWO VALUES (100F-90F = 10F DELTA T)
C TO F CONVERSION (C*1.8) + 32 = F
F TO C CONVERSION (F - 32.0) / 1.8 = C
LBS * 0.453592 = KILOGRAMS
KILOGRAMS * 2.204623 = POUNDS
GALLONS * 3.785412 = LITERS
LITERS * 0.264272 = GALLONS
QUARTS * 0.946353 = LITERS
LITERS * 1.056688 = QUARTS
Sticking a nail in the project.
Boeing abandones starliner after loses
Boeing has not abandoned the Starliner program after experiencing significant financial losses. The company continues to evaluate options to salvage the program, including potentially operating a cargo mission to test fixes to the propulsion system. Boeing is still considering how to address the propulsion issue and has not publicly announced plans to abandon the program. The company is working on resolving the issues and is exploring options to recover financially.
History of why we are here:
Following the Space Shuttle Columbia disaster in 2003, President George W. Bush announced the Vision for Space Exploration in 2004, which started the transition away from the Space Shuttle and toward new deep-space exploration programs. However, the program announced in 2004 was the now-canceled Constellation program—not Artemis. The Space Shuttle did not fully retire until 2011, and the Artemis program was not established until 2017.
2004: Vision for Space Exploration and the Constellation program
The decision:
In January 2004, after the loss of Space Shuttle Columbia and its crew, President Bush announced the Vision for Space Exploration. This initiative called for the Space Shuttle fleet to be retired after completing assembly of the International Space Station (ISS).The goal:
The Vision set out a plan for developing a new crewed vehicle to return humans to the Moon and later travel to Mars and beyond.The program:
The Constellation program was formed in 2005 to fulfill this vision. It involved the development of two new launch vehicles, the Ares I for crew and the Ares V for cargo, as well as the Orion crew capsule and the Altair lunar lander.
The path from Constellation to ArtemisConstellation's cancellation:
Following an independent review that found Constellation to be over budget and behind schedule, President Barack Obama formally canceled the program in 2010.The start of Artemis:
In 2017, President Donald Trump established the Artemis program. The new program repurposed the Orion crew capsule from the Constellation program and adapted much of the launch hardware to create the Space Launch System (SLS).The end of the Space Shuttle
Final flights:
The Space Shuttle program continued flying missions to assemble the ISS after the 2004 announcement.Official retirement:
The program officially ended with the landing of Space Shuttle Atlantis on July 21, 2011. A six-year gap followed where American astronauts relied on Russian Soyuz vehicles to get to the ISS, before the Commercial Crew Program began.
The Artemis III mission in the meantime
Artemis II will be NASA's first crewed flight around the moon since Apollo 17 launched in 1972 (albeit one surrounded by questions, with some people wondering if humanity's return to the moon is doomed). It will carry four astronauts aboard the Orion spacecraft on a roughly 10-day journey. The selected crew consists of pilot Victor Glover, commander Reid Wiseman, and mission specialists Jeremy Hansen and Christina Koch. Originally scheduled for 2024, the mission has been delayed to no earlier than February 2026 — possibly even April 2026. The engineers must work through several technical issues uncovered after the uncrewed Artemis I flight. During that 2022 mission, Orion's heat shield performed its job but experienced unexpected erosion, prompting a deep review of how its material responds to extreme re-entry temperatures. NASA isn't taking chances. The shield must survive 5,000-degree Fahrenheit re-entry conditions with human lives aboard.
Beyond the heat shield, Orion's life-support and power systems have faced additional scrutiny. Problems with the environmental control unit (responsible for maintaining cabin air and temperature) and internal batteries led NASA to extend testing cycles into 2025. Meanwhile, ground systems at Kennedy Space Center, including fueling and crew access platforms, underwent upgrades to improve reliability. Each fix demands new simulations, inspections, and certification before astronauts can climb aboard.
NASA officials emphasize that schedule discipline cannot outweigh crew safety. The space agency prefers to stack the Artemis III hardware while Artemis II engineers methodically clear the final test milestones. As Artemis II commander Reid Wiseman explained (via Space.com), "We're going to launch when this vehicle is ready, when the team is ready, and we're going to go execute this mission to the best of our abilities." His words reflect NASA's broader mindset: Progress will continue, but the countdown won't begin until every system, and every person, is fully prepared.
As Artemis II undergoes its final checks, NASA is forging ahead with Artemis III, marking a bold step towards humanity's return to the moon. The agency began processing the mission's Space Launch System (SLS) core stage and twin solid-fuel boosters at Kennedy in mid-2025. According to NASA, technicians are already inspecting and stacking hardware components while the Orion crew capsule and European-built service module are being outfitted at separate facilities. The mission aims to deliver the first woman and next man to the moon's south polar region, though the agency hasn't published which astronauts will fill these historic roles.
Artemis III will rely on technologies tested by Artemis I and II, including Orion's navigation system and deep-space communication links. It will also depend on new commercial hardware, notably SpaceX's Human Landing System (HLS) Starship, which will ferry the astronauts from lunar orbit to the surface. Coordination between NASA, SpaceX, and international partners is intense, as delays in one program cascade into another. For now, though, NASA's eyes remain fixed on Artemis II. Only when that crew returns safely can we really increase what we know about Artemis III and NASA's return to the moon.
According to NASA, the Artemis III journey will represent one of the most ambitious feats of engineering and human skill ever attempted in deep space, though NASA also emphasizes the knowledge gained from prior flights. The mission aims to take astronauts to the lunar South Pole, a region of high scientific interest due to its water ice and unique geology. The crew's work there, including gathering samples and various data, will not only deepen our understanding of the moon but also serve to inspire the next generation of explorers, which NASA has already named the "Artemis Generation."
NASA opens SpaceX's moon lander contract to rivals over Starship delays
Duffy's comments follow months of mounting pressure within NASA to speed up its Artemis lunar program and push SpaceX to make greater progress on its Starship lunar lander, while China progresses toward its own goal of sending humans to the moon by 2030.
It represents a major shift in NASA's lunar strategy, starting a new competitive juncture in the program for a crewed moon lander just two years before the scheduled landing date. Blue Origin is widely expected to compete for the mission, while Lockheed Martin (LMT.N), opens new tab has indicated it would convene an industry team to heed NASA's call.
Starship, picked by NASA in 2021 under a contract now worth $4.4 billion, faces a 2027 moon landing deadline that agency advisers estimate could slip years behind schedule, citing competing priorities. Musk sees Starship as crucial to launching larger batches of Starlink satellites to space and eventually ferrying humans to Mars, among other missions."They do remarkable things, but they're behind schedule," Duffy said of SpaceX's lunar lander work, adding President Donald Trump wants to see the mission take place before his White House term ends in January 2029.
The move is a significant change under the agency's acting leadership, and as the White House and Duffy begin to reopen the nomination process for a permanent administrator. Billionaire entrepreneur and SpaceX customer-astronaut Jared Isaacman, an ally of Musk's, is in talks to reclaim his nomination that had been yanked by Trump over the summer.
Musk shrugged off the specter of more competition in a social media post.
"SpaceX is moving like lightning compared to the rest of the space industry," the SpaceX CEO wrote on X, replying to a user on Monday. "Moreover, Starship will end up doing the whole Moon mission. Mark my words."The mission involving SpaceX, Artemis 3, would be the first human lunar landing since Apollo 17 in 1972.
Bezos' space company Blue Origin, with its Blue Moon lander in development, has a similar lunar landing contract awarded by NASA in 2023 but for later Artemis moon missions. The company had protested NASA's initial decision to only pick SpaceX in 2021 and fought for years to convince the agency and lawmakers to select another proposal as a redundancy.
Duffy's reference to Blue Origin on Monday suggests Bezos' space company could contend for Artemis 3.
Blue Origin has been developing its Blue Moon lander in Florida with relatively little public attention under a contract worth roughly $3 billion. SpaceX has been developing Starship in Texas in a whirlwind campaign of test-to-failure demonstration missions, but NASA has grown uneasy with a lack of progress on lunar lander-specific development milestones.NASA's multibillion-dollar Artemis program is a series of missions involving multiple contractors aimed at returning humans to the moon for a long-term presence there. Artemis 3 has been planned for 2027 with SpaceX's Starship.
Artemis 2, opens new tab, a 10-day flight around the moon and back involving systems built by Boeing (BA.N), opens new tab, Northrop Grumman (NOC.N), opens new tab and Lockheed Martin (LMT.N), opens new tab, is on track for April and could get moved up to February, he added.
Bezos and Blue Origin CEO Dave Limp reportedly spoke with Trump over the summer when the Republican president was feuding with Musk, a supporter in the 2024 election who was tapped to lead efforts to cut the federal government known as DOGE.
The current approved annual Starship launch rate is 25, following an approval by the FAA in May 2025. This is a significant increase from the previous limit of five, and SpaceX's goal is to increase this further to a weekly launch cadence, which could be achieved in 2026. However, the actual launch rate has been much lower than the approved maximum, with a total of five orbital flights by mid-October 2025.
Approved rate:
The FAA has approved up to 25 annual Starship/Super Heavy orbital launches from the Boca Chica launch site.
Previous rate: Before the recent approval, the limit was five launches per year.Actual rate:
By mid-October 2025, only five Starship orbital launch attempts had been made, and no further launches were planned for the remainder of 2025.Future goal:
SpaceX aims for a launch rate of up to 48 per year (one launch per week), potentially starting in April 2026, contingent on resolving technical issues and achieving full reusability.
It will take more than 6 consecutive launches for refill and at least a flyby and ocen landing from a second that is to be the return taxi once showing it can land on the moon.
Opening was about "Unlimited Fresh Water: Can Glass Domes Save Us?" where the water evaporates within a small space and is cooled once it reaches the top sort of like a still.
Fact check: Are illegal immigrants eligible for ACA subsidies under current US law?
Checked on October 20, 2025
Executive Summary
Undocumented immigrants are not eligible for federally funded Affordable Care Act (ACA) Marketplace coverage or premium tax credits under current U.S. law; this is consistently stated across official guidance and recent analyses dated October 2025 through January 2026. Mixed-status households can enroll eligible, lawfully present family members and apply for subsidies on their behalf, but that process does not extend ACA subsidies to undocumented individuals themselves
Undocumented immigrants can't get a REAL ID, but may still qualify for other state papers
Noncitizens are not illegals as they like refugees are also not illegals.
Noncitizens’ Access to Health Care
NASA's chosen lander, SpaceX's Starship, may lose Artemis III moon landing contract
Time is ‘running out’ for SpaceX as Artemis III mission deadline looms, despite successful launch
China race and lagging progress Nasa thoughts of space x needs 10 to 20 more launchses before NASA will feel that its safe.
similar to Gravity topic that we have
AI Overview
Space Suit:
Requirements, Raw Materials & Components ...
A spacesuit has multiple layers that provide protection, including an inner Liquid Cooling and Ventilation Garment for temperature control, a pressure bladder and restraint layer for maintaining shape and holding oxygen, and an outer Thermal Micrometeoroid Garment (TMG) with multiple insulation layers and an outer shell to protect against radiation and micrometeoroids. Other materials like Nomex, Kevlar, and Teflon are used for heat resistance, durability, and abrasion protection.
Inner layersLiquid Cooling and Ventilation Garment (LCVG):
This is the innermost layer, worn closest to the skin. It's made of nylon spandex and contains tubes that circulate water to keep the astronaut cool.Pressure Bladder:
A urethane-coated fabric layer that holds in oxygen and creates the necessary pressure inside the suit.
Restraint Layer: This layer holds the bladder layer in shape and prevents it from ballooning outward under pressure. It is often made of a tear-resistant material like ripstop nylon.
Outer layers (Thermal Micrometeoroid Garment - TMG)Insulation layers:
Several layers of aluminized Mylar or Kapton are used, separated by a scrim material, to create a thermal barrier that works like a thermos to insulate the astronaut from extreme temperatures.Outer shell:
The outermost layer is designed for durability and protection. It is often made of a tough, ripstop fabric that can include materials like Ortho-Fabric, which contains Nomex, Teflon, and Kevlar to provide protection against tears, abrasions, and micrometeoroids. The outer layer is also white to reflect sunlight and hea
Lest we forget No More Kings...
What layers do you think should be present in a space suit that can provide:
1) air retention
2) radiation protection
3) temperature protection
5) pressure mainenance against vacuum
6) light weight
7) flexibility for movement (eg, fingers, legs, feet, arms, head)The forum archive contains a number of links, some quoted text, and plenty of opinion...
This new topic of RobertDyck's has the potential to become a repository of useful knowledge that a person wanting to create a space suit might consult.
Here is an index of the topics which contain some of this.
Spacesuit Compatibility Requirement
Spacesuits - Its about time we came back to them
Spacesuits - personal spaceship
New idea for Mechanical CounterPressure suit
The vehicle is supported by placing it into a payloaad shroud and needs intrgration to couple it to any rocket to which was the intent. Its to bad that space x is going to off load Falcon 9 making just the Atlas replacement the only option left for its future.
Excersise is a 2 fold item as we know fromthe cost of microgravity onboard the ISS.
So after oxygenation.
For people that are losing the mental ability one would set to make use of puzzles, coloring art or painting with a tablet.
The spacesuits will need many layers of materials, some strechy and for comfort while wearing the spacesuit.
edit to update:
Spacewalk Spacesuit Basics
NASA and Lockheed may launch Orion on new rockets are now exploring the possibility of launching Orion on rockets other than the Space Launch System (SLS).
Thats quite the about face.
This consideration marks a significant shift from previous plans, driven by ongoing challenges with the SLS program. The exploration of commercial launch vehicles for future missions could potentially reshape NASA’s approach to deep-space exploration.
Lockheed Martin has been the developer of Orion since 2006, making specific engineering decisions to ensure the spacecraft’s compatibility exclusively with the SLS. This included considerations of the spacecraft’s size and propulsion interfaces, which were tailored to fit the SLS specifications. The early assumptions of the Artemis program, starting in 2019, further cemented this relationship, with budget allocations exceeding $20 billion for SLS development through 2025, reinforcing the expectation that Orion would launch solely on SLS for lunar missions.
Potential Alternative Launch Vehicles
SpaceX’s Starship emerges as a leading candidate for launching Orion, given its successful test flights in 2025 and its impressive payload capacity exceeding 100 metric tons to low Earth orbit. NASA has already invested $2.9 billion in a Starship lunar lander variant, indicating a strong interest in leveraging SpaceX’s capabilities for future missions. This investment reflects the agency’s willingness to consider commercial partners as viable alternatives to the SLS.Blue Origin’s New Glenn rocket, scheduled for its debut in late 2025 from Cape Canaveral, presents another potential option. With the capability to handle Orion’s 26-metric-ton mass and a payload capacity of up to 45 metric tons to low Earth orbit, New Glenn could offer a viable alternative for launching Orion. The introduction of New Glenn into the market could further diversify NASA’s launch options, enhancing the agency’s ability to meet its exploration goals.
Additionally, United Launch Alliance’s Vulcan Centaur, operational since 2024, offers a medium-lift option that could be paired with upper stages for Orion missions. Backed by NASA’s $5.6 billion in national security launch contracts, Vulcan Centaur represents a reliable and tested alternative. These potential launch vehicles provide NASA with a range of options to consider as it seeks to optimize its Artemis program and achieve its exploration objectives.
Implications for NASA’s Artemis Program
Adopting alternative rockets could significantly accelerate the timelines for the Artemis program, potentially enabling crewed lunar landings by 2027 instead of 2028 under the current SLS constraints. Lockheed Martin is leading adaptation studies to explore these possibilities, highlighting the potential for more efficient mission planning and execution. This shift could also result in substantial cost savings, reducing per-launch expenses from SLS’s $4 billion to under $1 billion on commercial vehicles, while still preserving Orion’s role in the 10 planned Artemis missions through 2035.However, transitioning to new launch vehicles is not without risks. Certification processes for new vehicle pairings, including FAA and NASA safety reviews, are expected to take 18-24 months starting in 2026. These reviews are crucial to ensuring the safety and reliability of the new launch configurations, but they also introduce potential delays and uncertainties into the program’s timeline. Balancing these risks with the potential benefits will be a key consideration for NASA and its partners as they move forward.
Lockheed Martin’s Perspective and Next Steps
Lockheed Martin executives have expressed openness to evolving Orion’s launch architecture to meet NASA’s goals. Vice President Rob Binnie stated, “We’re open to evolving Orion’s launch architecture to meet NASA’s goals,” reflecting the company’s willingness to adapt to changing circumstances and explore new opportunities. Lockheed Martin’s $93 billion backlog in space contracts underscores the company’s significant role in the aerospace industry and its commitment to supporting NASA’s exploration efforts.Planned studies through 2026, including wind tunnel tests and simulations for Orion on non-SLS stacks, are funded by a $100 million NASA allocation. These studies aim to evaluate the feasibility and performance of Orion on alternative launch vehicles, providing critical data to inform future decisions. The potential for partnerships with commercial providers also presents opportunities for Lockheed Martin to collaborate with other industry leaders, sharing intellectual property for Orion’s avionics in alternative configurations.
The exploration of alternative launch options for Orion represents a significant shift in NASA’s approach to deep-space exploration. By considering commercial launch vehicles, NASA and Lockheed Martin are positioning themselves to overcome the challenges associated with the SLS program and capitalize on new opportunities for innovation and collaboration. This strategic pivot could ultimately enhance the Artemis program’s success and ensure the continued advancement of human space exploration.
I believe that we have a topic for Yuri day
The "Yuri's Night Mars Society" refers to The Mars Society's support for and participation in Yuri's Night, a global celebration of spaceflight that takes place annually on April 12th. The Mars Society, an international nonprofit organization dedicated to the exploration and settlement of Mars, uses the event to promote space education and STEM excitement, often participating in local celebrations or encouraging members to host their own events.
Yuri's Night: This is a worldwide annual event celebrating spaceflight history on April 12th, commemorating both Yuri Gagarin's first human spaceflight in 1961 and the first Space Shuttle launch in 1981.
The Mars Society's involvement: The Mars Society has a history of partnering with Yuri's Night events to promote space and STEM activities.
Event types: These can include large public events at museums and NASA centers, as well as smaller, community-based gatherings like parties, movie screenings, or barbecues.
Goals: The collaboration aims to spark interest in space exploration and education, particularly focusing on future human journeys to Mars
https://www.marssociety.org/topics/yuris-night/ 2019
What is Crunch wrap?
"Crunch wrap" is the informal name for a new material SpaceX is testing on Starship to seal gaps between heat shield tiles during atmospheric reentry. This material, often a ceramic fiber felt, is installed around each tile before it's snapped into place. After installation, the excess material is trimmed, creating a flush and sealed surface that prevents hot plasma from leaking through the gaps and damaging the underlying layers.
Why it's needed
Heat leakage: In previous flights, heat was able to seep through the gaps between the heat shield tiles, causing the underlying ablative material to burn away and creating white deposits on the hull.
Durability: The "crunch wrap" is designed to be quickly trimmed and allows the tiles to be more resistant to damage during reentry and to better withstand the stress of multiple flights without extensive refurbishment.
Rapid reusability: By improving the sealing and reliability of the heat shield, the "crunch wrap" helps SpaceX achieve its goal of making Starship a rapidly reusable vehicle.
How it works
Installation: Before a tile is mechanically attached, the "crunch wrap" material is wrapped around its sides.
Sealing: When the tile is pressed into place, the material is forced into the gaps between the tiles.
Trimming: The excess material that sticks out beyond the surface is then cut off, leaving a neat, flush seal.
Testing: This system was tested and performed well, leading SpaceX to plan on using it more extensively on future flight
Flight 11 Crunch Wrap™ TPS upgrade

We also know that the ring of satelites are also pushing it outward making it farther away than it was.
I see that the free trial period is over and the cost will only rise since the government is going to make use of more of those Azure servers for cloud based systems from what I have heard.
As for the hosting the society that requires being able to set up equipment to process and not just be a buffer for the media coming from the convention.
related sub topic for Mars index of what we have for clues to what is going on for Earth.
Magnetizing Mars - Creation of a Martian Magnetosphere
Artificial Magnetosphere - Electromagnetic Induction
Mini magnetosphere radiation shielding for a manned mission
As seen from beyound orbit
Seen a bit more closer
Vast Anomaly in Earth's Magnetic Field Keeps Growing, Satellites Reveal
A giant dent in Earth's magnetic field is continuing to expand, according to the latest data from a trio of satellites monitoring our world.
It's called the South Atlantic Anomaly, stretching across the gulf that separates Africa from South America, and the latest data suggests that it has expanded by roughly half the size of continental Europe since 2014, while its magnetic intensity weakens.
The measurements indicate that the ocean of molten iron in Earth's outer core, which generates the planetary magnetic field, isn't steady and calm but churning and complex, with behavior that can change the external field on timescales as short as years.
Earth's magnetic field is a vast web of magnetic field lines generated by the planet's core dynamo: the rotating, conductive, convecting fluid in the outer core that converts kinetic energy into magnetic energy. It stretches out into space, forming an invisible structure around our planet that helps keep the atmosphere in and cosmic rays out.
Over the eons, the magnetic field has fluctuated in intensity, even flipping entirely in complete polar reversals. These events pose no direct hazard to life on the surface, but there are other reasons to study them.
Some navigation systems rely on Earth's magnetic field, for example. The magnetic field also deflects charged particles; a weaker magnetic field makes satellites more vulnerable to hazardous charge buildup.
What's more, the magnetic field deflects solar and cosmic radiation, so astronauts and people flying at high altitudes are exposed to higher radiation doses where the magnetic field is weaker.
Understanding changes in the magnetic field can reveal what's happening deep inside our planet, which, in turn, may help scientists build better predictive models of future behavior to mitigate these problems.
The size and strength of the anomaly in 2014 (top) and 2025 (bottom). (ESA)The South Atlantic Anomaly, or SAA, has been known since at least the 1960s, but there were no detailed, continuous studies on it until the launch of ESA's Swarm mission in 2013 – three satellites designed to work together to map the geomagnetic field.
The latest results of the Swarm mission represent the longest continuous monitoring of Earth's magnetic field to date, revealing new complexities to the SAA.
"The South Atlantic Anomaly is not just a single block," says geophysicist Chris Finlay of the Technical University of Denmark. "It's changing differently towards Africa than it is near South America. There's something special happening in this region that is causing the field to weaken in a more intense way."
Scientists don't know exactly what's causing the anomaly, but they do know that the magnetic field inside the planet below that region is not behaving as expected. Earth's magnetic field is roughly dipolar; the north magnetic pole is where magnetic field lines dive into the planet, and the south magnetic pole is where they emerge.
This is a very simplified version; the magnetic field as a whole is rather more complicated, but by and large, this model describes how the field is expected to behave. At the SAA, some of the magnetic flux beneath Earth's surface is curiously reversed.
"Normally we'd expect to see magnetic field lines coming out of the core in the southern hemisphere. But beneath the South Atlantic Anomaly we see unexpected areas where the magnetic field, instead of coming out of the core, goes back into the core," Finlay explains.
"Thanks to the Swarm data we can see one of these areas moving westward over Africa, which contributes to the weakening of the South Atlantic Anomaly in this region."
This magnetic flux reversal could be linked to a large, mysterious blob of super-hot material outside Earth's core known as the African Large Low-Shear-Velocity Province (LLSVP) under the SAA.
That blob could disrupt convection from the core, which in turn would change the behavior of the magnetic field above it. It's thought that this is a normal Earth behavior; we just didn't have the tools to study it until recently.
Other changes Swarm has observed in Earth's magnetic field include a slight weakening over Canada and a slight strengthening over Siberia, linked to a shifting magnetic structure underneath North America.
"It's really wonderful to see the big picture of our dynamic Earth thanks to Swarm's extended timeseries," says Anja Stromme, Swarm mission manager at ESA. "The satellites are all healthy and providing excellent data, so we can hopefully extend that record beyond 2030, when the solar minimum will allow more unprecedented insights into our planet."
SpaceNut,
If we're going to add that much metal to an already energy-intensive device like a photovoltaic cell, why not build a simpler and more robust solar thermal concentrator?
AI Overview
On average, a U.S. home consumes approximately 1.2 to 1.25 kilowatt-hours (kWh) per hour. This figure is an average calculated from yearly data and represents the overall rate of energy usage, but actual consumption varies throughout the day and seasonally.
For instance, the average 2022 annual consumption of electricity was 10,791 kWh per household.
10,791 kWh per year / 365 days = ~29.56 kWh per day
29.56 kWh per day / 24 hours = ~1.23 kWh per hour
Factors affecting average hourly electrical use
Hourly electrical usage fluctuates significantly depending on several factors:
Time of day: Demand for electricity is typically highest during the afternoon and evening hours when occupants are home, cooking, and using appliances like air conditioning.
Season and climate: A home's biggest energy drain is typically from heating or cooling systems. Homes in hot climates use more energy for air conditioning in the summer, while those in cold climates use more for heating in the winter.
Appliance usage: The average hourly consumption changes depending on which appliances are being used. High-wattage devices like air conditioners, electric ovens, and clothes dryers consume significant power when running.
Household size: A larger household typically has more occupants and appliances, leading to higher overall energy use.
For a more accurate comparison, the U.S. Energy Information Administration (EIA) notes that a single-family detached home in the South consumes much more electricity than an apartment in the Northeas
That said we need to store and regulate power output at the sizing for the concentrator based on inconsistent daily input of solar energy collection hours.
AI Overview
Concentrated solar thermal (CST) energy is not feasible for residential electricity generation due to its high cost and complexity. It is almost exclusively used for large-scale, utility-level power plants. For a U.S. home, the standard solution for converting sunlight into usable electricity is a photovoltaic (PV) panel system, typically including battery storage.
Here is a BBCode guide on how to size a residential solar PV system based on average hourly electrical consumption.
Sizing Residential Solar Photovoltaic (PV) for a U.S. Home
For the average U.S. home, which uses roughly 30 kWh per day, a solar PV system will need a capacity of around 6 kW. This can vary significantly depending on your location, lifestyle, and home size.
Step 1: Determine Your Hourly and Daily Energy Needs
Locate your total energy usage: Review your last 12 months of utility bills to find your annual kilowatt-hour (kWh) usage. Using a year's worth of data accounts for seasonal spikes, such as higher air conditioner use in summer.
Calculate your daily average: Divide your total annual kWh by 365 to get your average daily consumption.
Estimate your hourly usage: Divide your daily average by 24 hours to find your average hourly consumption. However, note that a battery storage system is necessary to provide power during the night, as solar panels only generate electricity during daylight hours.
Step 2: Find Your Peak Sun Hours
Look up your location's peak sun hours: Use a map or a tool from the National Renewable Energy Laboratory (NREL) to find the average number of "peak sun hours" per day in your area. These are the hours where the solar intensity is high enough to generate the maximum power from your panels.
Step 3: Calculate the Required System Size (in kW)
Calculate the ideal daily output: Divide your average daily kWh usage by your area's peak sun hours.
Add a buffer for inefficiency: Multiply the result by 1.2 (or 120%) to account for energy losses from the wiring, inverter, and system degradation over time. This gives you the size of the system in kilowatts (kW).
Consider future use: If you plan to add a new electric vehicle or appliance, increase your system size to account for the additional load.
Step 4: Estimate the Number of Panels
Find your panel wattage: Look up the rated wattage (W) of the specific solar panels you are considering. A common residential panel has a wattage between 300W and 450W.
Determine the number of panels: Divide your required system size (in watts) by the panel's wattage.Required System Size (in watts) / Panel Wattage (in watts) = Number of PanelsNote: A 1 kW system is 1,000 watts.
Step 5: Account for Energy Storage
Determine battery needs: For full backup power, your battery storage capacity (in kWh) should roughly match your average daily energy consumption. For example, a home using 25 kWh daily might start with a 10–15 kWh battery and expand later.
Consider discharge rate: Batteries have a discharge rate that affects how many appliances can be run simultaneously. This is especially important for running heavy-duty items like an air conditioner.
Example Calculation for an Average U.S. Home
Assumptions:
Daily Consumption: 30 kWh
Peak Sun Hours: 5 (varies by location)
Panel Wattage: 400 W
Calculation:
Required Power Output: 30 kWh / 5 h = 6 kW
Adjusted for Inefficiency: 6 kW x 1.20 = 7.2 kW
Required Number of Panels: (7.2 x 1,000 W) / 400 W = 18 panels
Approximate Battery Storage: ~25 kWh for a full day of backupAI Overview To size a solar thermal concentrator for a daily thermal energy demand of 40 kWh, you need to consider several key variables, most importantly the average daily peak sun hours for your specific location. The aperture area, or the size of the collector, is directly dependent on the amount of available sunshine and the system's efficiency. Calculation overview The general formula to find the required aperture area of the concentrator is:\(Area=\frac{Total~Daily~Energy~Required}{(Solar~Irradiance)\times (System~Efficiency)}\)Here is a breakdown of the steps involved in the calculation.
Step 1: Determine average daily solar irradiance Find the average daily peak sun hours for your location. This is a measure of the amount of solar radiation available per day, often expressed in \(kWh/m^{2}/day\). You can find this data from solar radiation maps or resources like the National Renewable Energy Laboratory (NREL). Example: For a location with 5 peak sun hours, the daily solar irradiance is approximately \(5~kWh/m^{2}/day\).
Step 2: Estimate system efficiency The overall efficiency of a concentrating solar thermal system can vary based on several factors, including: The type of concentrator (e.g., parabolic dish, trough).Optical losses from reflections and the receiver.Thermal losses from the receiver to the environment. For a preliminary estimate, a thermal efficiency (Eta) of about 80% is a reasonable starting assumption. It is important to note that this is a conservative value; a real-world system will have many loss factors. You may also need to budget for additional losses, such as a 20% overhead, to account for real-world inefficiencies.
Step 3: Calculate the required collector area Using the daily energy demand of 40 kWh, the location's average daily solar irradiance, and the estimated system efficiency, you can calculate the required aperture area. Formula:\(Area~(m^{2})=\frac{40~kWh}{(Peak~Sun~Hours~in~kWh/m^{2})\times (Efficiency)}\)Example calculation:Let's assume your location has an average of 5 peak sun hours (\(5~kWh/m^{2}/day\)) and you estimate a system efficiency of 80% (0.80). \(Area~(m^{2})=\frac{40~kWh/day}{(5~kWh/m^{2}/day)\times (0.80)}\)\(Area~(m^{2})=\frac{40~kWh/day}{4~kWh/m^{2}/day}\)\(Area~(m^{2})=10~m^{2}\)In this example, you would need a concentrator with an aperture area of approximately 10 square meters. Additional factors for refined sizing For a more precise sizing, consider these additional factors:
Seasonal variation:
Your calculation is based on an average day. Energy production will be higher in summer and lower in winter. For consistent year-round performance, you must size the system based on the minimum sun hours for your location.Tracking systems:
A concentrator's performance is highly dependent on how well it tracks the sun. One-axis or two-axis tracking systems will yield more energy than a stationary collector, but also increase complexity and cost.Thermal storage:
Storing excess thermal energy in a tank allows you to use the energy when the sun is not shining. The storage size should be matched to your usage patterns and the solar field to optimize daily operation.Collector type:
Different concentrator designs have different efficiencies and space requirements. Common types include parabolic troughs, dishes, and linear Fresnel collectors.Safety factors:
It is often wise to oversize the system slightly to account for cloudy days, system degradation over time, and other inefficiencies
we have many posts about this size of reactor that puts out to much power
AI Overview
What Are SMRs: What Small Modular Reactors Are And Why They ...
Small modular reactors (SMRs) are advanced nuclear reactors with a power output of up to 300 megawatts that are designed to be factory-built as modules and then transported to a site for assembly. They offer potential benefits like streamlined construction, greater scalability, flexibility in siting, and enhanced safety features that often rely on passive cooling systems. SMRs are envisioned as a way to provide carbon-free energy for various applications, including powering communities, industrial facilities, and data centers, and can be deployed in configurations to match energy demand.
Functionality and technology
Power output: SMRs have a capacity of up to 300 MWe, about one-third of a traditional nuclear reactor, with some designs as small as 1-10 MWe.
Nuclear fission: Like traditional reactors, SMRs use nuclear fission to generate heat, which can then be used to produce electricity or for other industrial applications like desalination.
Modular construction: Components are manufactured in a factory and then shipped to the site, which is intended to reduce construction costs and time compared to large, custom-built plants.
Scalability: SMRs can be deployed in single or multi-module configurations to meet varying energy needs, a concept called "economy of multiples".
Advantages and benefits
Flexibility: The smaller size allows for siting in a wider range of locations where large plants might not be feasible.
Safety: Many designs incorporate passive safety systems that rely on natural processes, like convection, for cooling, which reduces the reliance on active mechanical components.
Cost and time: The goal is to achieve lower initial capital costs and faster deployment timelines through factory production and standardization.
Versatility: Beyond electricity generation, SMRs can be used for process heat, water desalinization, and other industrial applications.
Carbon-free energy: As a nuclear technology, SMRs provide a source of reliable, carbon-free power.
Challenges and considerations
Economic viability: While proponents aim for cost savings, some projects have faced significant cost overruns, and it is unclear if the "economy of multiples" will be cheaper than economies of scale for large plants.
Deployment: As of mid-2025, only a few operational SMRs exist, primarily in Russia and China, and many proposed designs are still years away from deployment.
Safety claims: The effectiveness of passive cooling systems is dependent on proper manufacturing and could be affected by environmental factors or defects.
Regulatory hurdles: SMRs face the same regulatory processes as traditional reactors, which can be a complex and lengthy challenge
but it seems that the miltary wants to cut the fuel strings that bind setting up bases.
Nuclear microreactors are smaller, factory-built power systems that use the same basic principles as traditional nuclear plants but at a fraction of the size. Most produce between one and 20 megawatts of electricity — enough to power a small town or a military installation — and can operate for years without refueling.