Improvements in Stirling Engines have made them a critical part of the future of space exploration and colonization. The Terran Space Academy reinforces the concepts of Power, Energy, Force and Momentum then brings you up to date on how a Stirling Engine functions and how they are being used in the space industry and throughout the world for power generation and cryocooling. Generating power in space is a critical component of survival. Complete loss of power in space is almost always fatal. The efficiency of you power generation system will determine how much of the available power you can use. Understanding power generation systems will be vital to your selection and success in the space industry. First let’s make sure we are on the same page when we talk about power. We will define power, energy, work, and force. Then we will apply our understanding to a power generation system. The main difference between an internal combustion engine and a Stirling engine is that the internal combustion engine takes in air for oxygen to burn with fuel, then expels the exhaust into the environment. This won’t work well in space. The Stirling engine uses two chambers, one hot and one cold, that have a gas sealed inside it and a regenerator or heat exchanger between them. The engine pumps heat from the hot end to the cold end putting pistons in between to make the heat energy accomplish work. The heat energy is converted to mechanical energy by the piston system and the mechanical energy is converted into electricity by putting coils and permanent magnets in the right place on the engine. If we heat one end of a Stirling engine the gas sealed in the engine will expand and move a piston, compressing the gas at the other end of the piston, this causes that area to radiate heat and then cool down. The compressed colder gas will then be allowed to flow around to the hot end, which has now expanded and cooled, the cold gas absorbs heat and starts to expand, and the cycle starts all over. The principles are the same for power generation. In this device electrical power is applied to move heat against a gradient and cool something down. This engine can also be used as a refrigerator by using electrical energy to pump heat away from something and make it colder than the environment. No matter how much heat you have if you don’t have a cold place to move it to you can’t get energy from the system. When charging our carbon dioxide batteries on Mars we have to have somewhere with less carbon dioxide to put it so we can discharge the batteries. Our gravity battery quits working when our weight hits the ground and our heat engine stops working if both sides of our Stirling engine are the same temperature. Why can’t we just use thermocouples like the RTG we talked abou ... https://www.youtube.com/watch?v=KKnu73DJbEQ
Understanding How the Raptor Rocket Engine Works!
The Terran Space Academy walks you through the design and components of the amazing full-flow staged combustion Raptor rocket engine!
Extra Credit: https://arc.aiaa.org/doi/full/10.2514/1.B38037
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Music Credits
Lost Frontier by Kevin MacLeod is licensed under a Creative Commons Attribution 4.0 license. https://creativecommons.org/licenses/by/4.0/
Source: http://incompetech.com/music/royalty-free/index.html?isrc=USUAN1300039
Artist: http://incompetech.com/
...
https://www.youtube.com/watch?v=5FjUv-VNcPg
China is on track with its three-phase plan to have a lunar base by the 2030s, while NASA's Bill Nelson has said the US will do the same by the 2040s. The United States has become so complacent that we don't even appoint knowledgeable people to powerful positions any longer.
If China controls cis-lunar space, how likely is it that American or European spacecraft will get clearance to land?
Let's look at China's progress on their International Lunar Research Station,
and listen to the latest brilliant exchange between American politicians.
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Credits
ESA
ULA
NASA
CNSA
SpaceX
...
https://www.youtube.com/watch?v=l-fkL8oUPBo
The Flight Termination System has been installed and Starship 24 is go for launch!
History will again be made in Texas! Ad Astra Pro Terra!
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https://www.youtube.com/watch?v=WzsFN4JYfxA
The Starship is the most innovative spacecraft ever conceived.
The Terran Space Academy provides an in depth analysis of the technology behind the Starship, to see if we had the technology to do this almost half a century ago, analyzing the closest analog produced by NASA. Comparing available rocket engines and fuels with a lesson on vacuum optimization, hydrogen energy production and efficiency, and methane fuel cells.
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Could the second stage of the Saturn V been modified to have flown like the Starship?
And come back to land?
Re-landing a spaceship is not easy.
The Saturn V 2nd stage was called the S II. It was hydrogen powered.
The only reusable hydrogen powered rocket flying today is the New Shepard by Blue Origin.
The New Shepard is not a large spacecraft, but it does reach the von Karman line.
Here you see it in action…
And here you see the landing legs deploying.
The New Shepard works well for suborbital flight, but it is quite small with, a mass of only 20,500 kg without fuel, and about 75,000 kg with fuel, according to Astronautix.
The Starship is much larger than the New Shephard. At 50 meters in height and 18 meters in diameter with a gross mass 1,320,000 kg it is the largest second stage ever built and is more than 17 times the mass of New Shepard. There is no real comparison between these two.
But the Saturn V second stage, built by North American Aviation, had a height of about 25 meters and a diameter of 20 meters. It had a dry mass of 36,200 kg and could hold 443,000 kg of propellant with a total gross mass of about 480,000 kg. It was called the S II and we’ll refer to it that way.
At more than one third the mass of the Starship we can start comparing these.
The S II had 5 of these hydrolox engines called the Rocketdyne J-2 with a vacuum thrust of 1,033 kilonewtons each and a specific impulse of 421 seconds in vacuum. Pause for a second. The BE-3 hydrolox engine used by Blue Origin on the New Shephard has a thrust of 490 kilonewtons and a vacuum thrust of 710kn. This does not seem like a great improvement. It can be throttled down to just 89kn which is good for landing.
And vacuum thrust and efficiency is not sea level thrust and efficiency. Some sources report the sea level efficiency of the J2 to be only 200 seconds while the vacuum is 421 seconds. I found this hard to believe but when I double checked my equations showing force (1,033N) divided by ejection velocity (Is*g=421sec*9.81m/s^2) equals mass fuel flow (250kg/s). Then assuming the same fuel flow at sea level takeoff with the thrust given by Rocketdyne at sea level of 486kN. Dividing this by the same fuel flow we get 198 seconds. This shows that vacuum optimized engines don’t work well at sea level.
But the J2 was
...
https://www.youtube.com/watch?v=5zBg6lwj1_8
Terran R beats Falcon 9!
The Terran Space Academy evaluates the Terran R rocket to be built by Relativity Space,
and compares it to the SpaceX Falcon 9, showing that when it comes to mass to LEO and reusability, the Terran R will be a better rocket system.
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Credits
Ulysse Carion for the DeltaV Subway Map
SpaceX, Relativity Space, NASA and the Glenn Research Center
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https://www.youtube.com/watch?v=sWhqNmJiufc
Can the NASA Lunar Contract Help Blue Origin Beat SpaceX to the Moon?
The Race is On! Blue Origin has a chance to make up for lost time and prove once and for all that they are a capable space company.
Extra Credit: https://patents.google.com/patent/US7418814B1/en
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https://www.youtube.com/watch?v=99qAt_Znf28
Starship technicians, engineers, and scientists will be needed to build the off-world homes we will need to survive on the Moon, Mars, Titan and beyond. How do you decide what role is best for you?
The Terran Space Academy is dedicated to helping you understand the fundamentals of space science, so that you can have a bright future in the space industry.
This lesson will analyze the importance of pressure differentials in rocket engine design by comparing the performance of the first generation Raptor to the more advanced Raptor 2. In closing we will introduce Professor Gregory Chamitoff and his amazing SpaceCRAFT virtual design program.
We will also review the basics of...
Turbopump Pressure
Combustion Chamber Pressure
Throat Pressure as it relates to Area
Exhaust and Ambient Pressure
Nozzle Expansion Ratio
Sea Level vs Vacuum Rocket Engine Nozzle Considerations
Aerodynamic Drag and Aerodynamic Stress
Gravity Drag and Thrust to Weight Ratio
Thank you so much for watching!
Ad Astra Pro Terra
Credits
Professor Gregory Chamitoff, Astronaut and Visionary,
Lawrence Hargrave Professor of Aeronautical Engineering
at the University of Sydney, Australia
and a Professor of Engineering Practice
in the Aerospace Engineering Department
at Texas A&M University in College Station, Texas
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Special Credit to the Texas A&M Aerospace Engineering Department
https://engineering.tamu.edu/aerospace/profiles/gechamitoff-.html
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Extra Credit and Further Study
http://www.braeunig.us/space/propuls.htm#:~:text=For%20space%20engines%2C%20where%20the,the%20extra%20thrust%20it%20generates.
https://spaceflight101.com/spx/spacex-raptor/
https://apps.fcc.gov/els/GetAtt.html?id=273481
https://seitzman.gatech.edu/classes/ae4451/thrust_coefficient.pdf
...
https://www.youtube.com/watch?v=DwMZvLn-mRs
Getting to the Moon and Returning with Something Valuable!
Keep exploring at http://brilliant.org/TerranSpaceAcademy/
Get started for free, and hurry—the first 200 people get 20% off an annual premium subscription. This video was sponsored by Brilliant!
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https://www.youtube.com/watch?v=e_4EEaIEnvI
The upcoming SN420 SpaceX Starship flight will NOT be suborbital!
In this Space Brief the Terran Space Academy makes the argument that suborbital is not the correct way to describe the upcoming March flight of the SpaceX Starship SN420.
We walk you through the deltaV and altitude requirements of a stable low Earth orbit,
and show that Starship SN420 will exceed all of these parameters...
Far exceeding the capabilities of the Blue Origin New Shepard or the Virgin Galactic Spaceship Two.
Requiring the creation of a category to describe the upcoming flight.
Thank you so much for watching!
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https://www.youtube.com/watch?v=FRvnm4emZQ0