Questions tagged [design]
Questions about how space vehicles and related hardware are designed. See also [structural-design] and [engine-design].
231
questions
6
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1answer
100 views
Why does the Perseverance rover have such complicated shaped spokes in its wheels?
Phys.org's NASA's Perseverance Mars rover gets its wheels and air brakes has some interesting photos includes some nice photos and below I've included a cropped section of a photo of one of ...
0
votes
1answer
109 views
Bipropellant RCS systems: Do they go together with docking? Or with manned spaceflight?
In a recent discussion, I asked about using a certain bipropellant system for RCS thrusters (I was actually thinking about it as fuel for an MMU jetpack or the "scooter" commonly imagined in science ...
3
votes
0answers
93 views
Are black and white stripes any better than uniform gray for thermal control?
Q: What color is a spaceship?
Several answers and comments on Why were Europe's first few satellites so stylish? Why the pronounced alternating white and black stripes? contain phrases like "thermal ...
2
votes
0answers
43 views
What is the load path for thrust in a rocket engine? [duplicate]
This may be a duplicate of this question but I wasn't sure if I could hijack that one to clarify or regenerate interest there.
What is the distribution of axial force in a combustion chamber? My ...
3
votes
1answer
161 views
What are common rocket fuselage designs?
I am wondering about the basic design considerations when building a rocket body.
is it made as a separate hollow cylinder with standalone tanks inserted inside?
is it made so that the tank walls are ...
1
vote
0answers
78 views
What is the limit to which we can scale up uniformly in all directions Space Shuttle SRB before it becomes unable to take off?
Let's say we like the Space Shuttle design so much, we want to use it as a reference for our new rocket. But we want to build rocket which will be capable of launching larger payload into Earth's ...
3
votes
1answer
105 views
Are few kilogram RTG's possible with similar mass-specific power to current designs?
This answer to Mass ratio of solar-electric versus radioisotope thermo-electric power for propulsion; beyond how many AU do RTGs win? estimates a crossover at about 4.3 AU, so a trip to the outer ...
8
votes
1answer
221 views
Why do Soviet and Soviet-derived rockets hot-stage instead of using ullage motors?
I am only aware of one US rocket that used hot-staging for maintaining proper ullage during stage seperation--the Titan family. Otherwise, US rockets tend to use reaction control systems or small ...
6
votes
0answers
166 views
Why is the diameter of the boosters of some launch vehicles smaller than the diameter of their payload fairing?
Whilst watching yesterday's Starliner launch I've noticed how skinny that Centaur (3.1m) looks compared to the CST-100 (4.5m).
Looking up the Atlas V I was amazed to find out that it has even larger (...
3
votes
4answers
238 views
Have there been any spacecraft designs with a bilaterally asymmetric cockpit?
One of the things that makes the Star Wars films so visually distinctive is the asymmetric spaceships, for example the Millennium Falcon below whose cockpit is located in the top right corner as ...
5
votes
0answers
93 views
How does the SpaceX Dragon nosecone separate?
SpaceX's Dragon uses a nosecone to protect the docking port during ascent.
The nosecone seems very large. 1/3 of the capsule's height large. And yet, it separates while the second stage engine is ...
5
votes
1answer
127 views
Mass ratio of solar-electric versus radioisotope thermo-electric power for propulsion; beyond how many AU do RTGs win?
Solar-electric propulsion has been used several times now in deep space missions. This question explores the scalability in comparison to Radioisotope thermoelectric generation or other nuclear-based ...
3
votes
1answer
145 views
Falcon 9 Type Rocket with Raptors
I've seen the question "Why don't SpaceX just use Raptors in the F9 now since their better" asked here and there, and I understand why it isn't possible to do that- they're not a drop-in replacement ...
5
votes
1answer
253 views
Why was the nose cone on the Space Shuttle's external tank pointy?
Inspired by comments under this answer to this question
Just how pointy does a rocket's nosecone need to be? (see also Why are the nose cones of current spacecraft less pointy?)
Why was the ...
23
votes
2answers
5k views
Is the mass of paint relevant in rocket design?
(Prompted by this answer):
Do the designers of large rockets* (have to) take the mass of the exterior paint into account?
If so, do we have examples of actual design changes/decisions based on this (...
2
votes
1answer
132 views
Does any US rocket, historical or current, besides those using LH2 as fuel apply thermal insulation for propellant?
Besides those using LH2 in a booster and/or sustainer stage, that is.
EDIT: I should have made it clear that this applies to launch vehicles, not spacecrafts flying deep space mission.
EDIT: OK, I ...
3
votes
0answers
108 views
Why is the relative axial position of oxidizer vs fuel tank inverted in the upper stages of most rockets?
In the first stages of most rockets, e.g. Atlas V, Delta IV and Falcon 9, the oxidizer tank is stacked on top of the fuel tank, with the usual explanation that such an arrangement gives the rocket a ...
2
votes
2answers
109 views
Are large spin gravity spaceships practical considering strength of materials
Are spaceships using spin-gravity to simulate normal earth gravity on their inner surface practical considering materials available today (i.e., steel, carbon fibre, etc.)? Imagine the
spaceship as ...
3
votes
1answer
135 views
Are these sliding ullage bulkheads in the OTRAG rocket? How do they seal?
This answer to Were there any non-state organizations to organize space flight and colonizations in the second half of the 20th century? mentions OTRAG and links to Astronautix's OTRAG page.
The ...
6
votes
1answer
113 views
What is “additional line load” [N/mm] for the Ariane 5 launch vehicle?
In the textbook Spacecraft Systems Engineering 4th ed. page 14, table 2.1 ("Acceleration values for the Ariane 5 launch vehicle") provides data on the loading of the Ariane 5 spacecraft. One of the ...
26
votes
2answers
2k views
Why aren't RCS openings an issue for spacecraft heat shields?
A spacecraft which needs to both maneuver and enter the atmosphere needs both a reaction control system and a thermal protection system (aka heat shield). As the heat shield needs to be on the outer ...
5
votes
2answers
182 views
How does Orbex save structural weight by using coaxial tanks?
British aerospace company Orbex is developing a small orbital rocket called Prime, which uses propane and liquid oxygen in two coaxial tanks.
One key aspect of propane is that it remains liquid at ...
1
vote
2answers
168 views
Saturn I's four outer engines' gas generator exhaust, why not vent to the side like the four inner engines?
At about 04:58 in Scott Manley's new video NASA Might Be Giving Away A Saturn I Rocket - Here's Why I Love This Vintage Booster he says:
So the four engines in ...
8
votes
3answers
701 views
Did von Braun have “a thing” for fins? Why did Saturn I block 2 get fins because it's a “von Braun” rocket?
At about 05:55 in Scott Manley's new video NASA Might Be Giving Away A Saturn I Rocket - Here's Why I Love This Vintage Booster he says:
So the Saturn; the first ...
11
votes
4answers
1k views
Are there liquid fueled rocket boosters having coaxial fuel/oxidizer tanks?
Reading this question, instead of stacking two tanks, are there boosters where tanks are coaxial, (like a thermos bottle) having a trussed or tridimensional structure between inner and outer tank?
...
25
votes
6answers
9k views
Why aren't rockets built with truss structures inside their fuel & oxidizer tanks to increase structural strength?
I've been wondering how a rocket fuselage can support all the weight of the upper stages when it is only made of a cylinder of very thin sheet metal. (Especially considering acceleration, vibration ...
7
votes
3answers
361 views
Why do all recent proposed lunar landers have payloads on top?
Every recently-proposed vacuum lander I've seen has its payload as far off the ground as possible. This necessitates cranes, ladders, and elevators to get things down. (Starship may be a partial ...
18
votes
3answers
2k views
How do these cubesats' whip antennas work?
This answer has identified the three 1U cubesats shown in the question, and links to Engineers Rule's Maya-1: The Philippines’ First CubeSat along with the video Animation of MAYA-1, The Philippines' ...
5
votes
1answer
150 views
What criteria dictate solar panel design?
On space craft equipped with solar panels, those panels comes with various form factors and number.
2 straight rows (e.g. progress, rosetta,...)
more straight rows (e.g. ATV, Juno,...)
only one ...
2
votes
0answers
70 views
Minimal heating a realistic reentry vehicle could achieve?
In this question, I asked whether it would be possible to make a reentry vehicle that could slow down from orbit and glide to the ground entirely passively. The answers and comments point out several ...
3
votes
3answers
275 views
Are there any designs of geostationary satellites available online?
Are there any designs of perhaps old geostationary satellites available online? After searching around I was mostly able to find either crude diagrams or designs for little cubesats, but nothing for ...
8
votes
1answer
220 views
Why have androgynous docking systems seemingly fallen out of favour?
There are two basic types of spacecraft docking systems:
Non-androgynous docking systems (examples: every U.S./Russian docking system currently in use for docking spacecraft) have two separate, ...
7
votes
1answer
272 views
Why aren’t rocket stages modular and interchangeable?
Being an avid player of Kerbal Space Program, it is intensely frustrating to return to the real world and have to remind myself that rocket stages can’t generally be swapped out between rockets (...
2
votes
0answers
101 views
What was the volume of the Space Shuttle orbiter, not just the crew cabin or cargo bay but the total volume of the entire craft?
For context, after an in-depth Google search, I asked the question "What was the volume of the Space Shuttle orbiter, not just the crew cabin or cargo bay but the total volume of the entire craft?" on ...
2
votes
0answers
38 views
Special Case Constellation Analysis Approach: Walker Constellation with Circular (e = 0) orbit in LEO
I am familiar with the general approach to propagate orbits using orbital parameters, and how to account for basic J2 perturbations. I am looking to perform some analysis on large walker ...
-1
votes
1answer
98 views
Was the Titan SRM thrust vs time curve engineered to allow for acceleration switches to initiate staging sequence events?
This answer describes the timing between the Titan III Stage 0 (SRM's) and Stage 1 events.
The Titan first stage ignited just prior to SRM separation:
Titan Stage I ignition occurs at ...
12
votes
2answers
2k views
How feasible is the Delta-Glider?
In Dr. Martin Schweiger's freeware spaceflight simulator Orbiter 2016, a very popular(but fictional) spacecraft is the Delta-Glider.
It is capable of take-off from a runway, has hover engines for ...
6
votes
1answer
161 views
How many motors on the new Mars 2020 rover? (and other questions)
With so many different motors on the new Mars 2020 rover, I'd like to ask if each motor programmed to operate independently or can the different motors operate in sync with each other?
Also, as a ...
8
votes
1answer
274 views
Why is multi-spool pump very rare on rockets?
The only one I know of is the LP LOX pump on RD-0120. A multi-spool design is already a default for jet engines, which are basically turbine-driven air pumps. A multi-spool pump can save at least the ...
12
votes
1answer
651 views
Why did the cones of the Mercury and Gemini capsules have a neck?
As highlighted by the green double-arrow lines in the pictures below, the Mercury and Gemini capsules had a (roughly) cylindrical "neck" at the end of the capsule cone. If they had instead followed ...
3
votes
1answer
56 views
Tradeoffs to consider for OBDH system design for a Multi-Spectral Imager payload? (Enceladus Mission)
I am having a problem with designing the On Board Data Handling (OBDH) system for our MSI (Multi-Spectral Imager) payload. Our payload will be detached from Orbiter and it will take photos (for ...
0
votes
1answer
86 views
How common are “parallel stages” in a launch vehicle?
I'm being told in this answer and in this comment that the fourth stage of the Farside rocketoon lies in the center of the four "cores" of the third stage.
See this answer for several pictures of ...
3
votes
4answers
680 views
Just how pointy does a rocket's nosecone need to be?
There are some beautiful images of the Qu8k rocket launch on this web page and I show a few below. There's a video (below) and the PDF Qu8k Final By Derek Deville, November 27, 2011
The stainless ...
1
vote
0answers
66 views
How does the inter-propellant seal works in kerosene/LOX and UDMH/NTO rockets?
I get that the inter-propellant seal on the SSME LOX HP pump is simply a series of cascading regular seals trying to eliminate bleed-through by venting and letting boil at each stage, so that when ...
2
votes
1answer
105 views
Are new precision gyroscopes used in spaceflight pretty much all optical?
Gyroscopes are used in spaceflight as parts of inertial systems to monitor spacecraft attitude. They are not absolute, they will drift slowly over time and so need occasional calibration via other ...
1
vote
0answers
44 views
How much more hardware is needed in a cross-fed CBC rocket than a non-cross-fed one?
Is it just a matter of adding a multi-in fuel manifold?
3
votes
0answers
148 views
Are LiPo batteries more suitable for 1st stage electric power than Li-ion batteries?
I've just ran across two mentions in Scott Manley's videos of LiPo batteries (Lithium-polymer) in first stage launch applications. These involve power levels of megawatts.
Why The Electron Rocket May ...
4
votes
1answer
190 views
What set of units does the Orion capsule cockpit instrumention use?
Shuttle was English, ISS is metric.
What's Orion?
For example: What units are inertial velocity displayed in?
1
vote
1answer
254 views
Why didn’t the space shuttle external tank have pressure-relief vents?
During a space shuttle abort, it would have been vitally important not to allow the vehicle to droop below 265 kilofeet during powered flight, as excessive aerodynamic heating below 265 kft would have ...
9
votes
1answer
503 views
Why are planetary probe RTGs tilted at a jaunty angle?
This image from here: Does the Dragonfly project (quadcopters on Titan) envision attached RTG's or would they be static and revisited for charging?
and this image
show that the RTGs on these two ...
