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Questions tagged [engineering]

Questions regarding the design or process of design of a spacecraft.

7 votes
0 answers
73 views

In mission planning, Δv estimates carry uncertainties due to navigation errors, propulsion variability, and orbital perturbations. What statistical methods are used to determine how much Δv margin to ...
Anushka_Grace's user avatar
10 votes
2 answers
2k views

Such as moons of the gas giants. I know the ice is as hard as rock but would it behave the same as regolith on Mars or the Earth’s moon?
Kasie Ream's user avatar
  • 3,052
0 votes
1 answer
209 views

I was wondering why aerospace engineers still have not ideated a way to produce heat shields which are larger in surface area so that a spacecraft during re-entry can aerobrake more efficiently as ...
Edoardo Porro's user avatar
10 votes
3 answers
2k views

The Webb telescope has a 5-layer sunshield, the thickest of which is 0.05 millimeters thick, and others are even thinner. I can not understand why it has to be extremely thin. this answer to Why was ...
Amir reza Riahi's user avatar
1 vote
0 answers
199 views

How was the approach to design different in the days of the Apollo program and today at SpaceX? I know that these are two different things that are difficult to compare. In any case, in both cases ...
Saturn V's user avatar
  • 1,457
3 votes
2 answers
1k views

I am calculating a jet - gas nozzle and to calculate it, I need to know the anisotropy of the air, what is it equal to? In this formula, the desired value is under the letter ...
DYNAMIC AEROSPACE's user avatar
1 vote
0 answers
203 views

Could anyone enlighten me with this puzzle ? The following frames are screenshots from an P&W RL10 engine's video. It's actually the top view of Fuel Injector Manifold and the LOX/Injector Domes (?...
user3184199's user avatar
1 vote
1 answer
267 views

There are a great many areas of application of PLD/FPGA in spacecraft. Let's take as a basis this classification of domains and subdomains, proposed in the November 24, 2023 FPGAInsights.com blogpost ...
ayr's user avatar
  • 383
2 votes
0 answers
125 views

I,ve been wondering if it was possible engineer and how we would we work it out DUAL preburner inline FFSCC ENGINE with concentric core and individual concentric turbine inside one another and maybe ...
AXGENT.INC INNOVATECH's user avatar
6 votes
4 answers
6k views

To what extent has internal insulation been tested to deal with the heat of re-entry? In the case of Starship, is the existing steel strong enough (to be non-ablative!), or would a different type of ...
Dagelf's user avatar
  • 757
1 vote
0 answers
158 views

For a story I'm working on, my characters have just docked with a space station in Low Earth orbit. It's set in the 2080s, so we're assuming no game-changing leaps of technology, merely what's ...
Hewholooksskyward's user avatar
7 votes
1 answer
229 views

I've been looking to build replicas of Apollo flight control hardware such as RHC, THC, ACA, TTCA and COAS, and am looking for detailed engineering drawings that show dimensions and internal ...
mini's user avatar
  • 547
6 votes
1 answer
937 views

I am looking for some document that summarizes all the aspects that need to be taken care of during design (structural resistance, life support system, thermal regulation, etc.). Something similar to ...
Saturn V's user avatar
  • 1,457
9 votes
1 answer
408 views

http://www.astronautix.com/m/mustard.html As described above, MUSTARD was a BAC project to develop a fully reusable VTO/HL shuttle to transport crew and payload to earth orbit. There were many ...
AnarchoEngineer's user avatar
32 votes
8 answers
8k views

I am curious what aspects of the Apollo program were impressive/advanced from an engineering perspective, in the 1960s and 1970s. That is, what would have made an educated engineer say, “Wow, they ...
adam.baker's user avatar
  • 1,074

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