Questions tagged [engineering]

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

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2
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1answer
66 views

Could a magnetic scoop work as a means to refuel a tank with hydrogen in orbit?

How effective would this be or would the Earth's magnetic field make it useless? Would it take too long for this to be of any use?
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1answer
107 views

What parameters drive the development effort and cost of a liquid rocket engine for orbital launchers(LEO - GEO)?

The development cost for a rocket engine drives the cost for a launcher and can be attributed to some basic parameters Apart from the few below, what others may be critical to developing and designing ...
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1answer
73 views

Where should ion drives be placed on a rotating space station of the lop-sided dumbbell variety?

I have been working on a model of a proposed artificial gravity facility by Joe Carroll, based on this paper. It is an initial concept paper and it doesn't spell everything out, so I am trying to ...
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2answers
75 views

Help Finding A Book

I am trying to find the book that contains the following chapter: https://www.faa.gov/about/office_org/headquarters_offices/avs/offices/aam/cami/library/online_libraries/aerospace_medicine/tutorial/...
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3answers
193 views

Is it possible to identify the main systems that would be present in a generalized space station?

What are the main parts of any space station? I have been making a 3D model of a hypothetical space station, and I'd like to ask if it is possible to identify some main components and/or subsystems ...
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2answers
2k views

How does the Saturn V Dynamic Test Stand work?

This photo instantly provokes a ton of questions in me: It shows the Dynamic Test Stand at Marshall SFC with the Enterprise, which was a Space Shuttle test vehicle, suspended for vibration testing. ...
8
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1answer
505 views

Sea level static test of an upper stage possible?

As we know that for the upper stages of the rocket, we need high propulsion efficiency thereby high specific impulse. For that we employ a nozzle with higher expansion ratios. Now, if we conduct the ...
21
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3answers
5k views

Why isn't there research to build a standard lunar, or Martian mobility platform?

While many terrestrial mobility platforms have been very successful, why are we spending millions to every rover device making it unique? Sure enough, different worlds offer different conditions, but ...
3
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1answer
121 views

What exactly are Tindallgrams? (spaceflight related)

The word "Tindallgram" appears in three posts: this answer to How complex was the math and physics necessary to place Apollo 11 on the moon? What is a “Lear Processor” and how did it work? this ...
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2answers
99 views

Would a nuclear turbojet with a chemical afterburner be a suitable intermediate between a pure nuclear turbojet and a nuclear thermal rocket?

NOTE: This is not the place to question the fundamental veracity of nuclear propulsion in aircraft and spacecraft. For context, in a spaceplane, the higher speeds you can attain under air-breathing ...
4
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1answer
373 views

How are umbilical connectors held in place until their intended detachment?

When a rocket is on its launch pad, umbilicals allow the flow of liquids, gases, electric power, and signals to the spacecraft. The umbilical is detached from the spacecraft at or before launch, to ...
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0answers
65 views

How is this engine put together? [duplicate]

I'm going through How to DESIGN, BUILD and TEST SMALL LIQUID-FUEL ROCKET ENGINES and am confused how their sample engine is physically built together. This is a picture of their assembly where the ...
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3answers
420 views

Overcoming the speed of light thanks to ion thrusters

I am wondering if I could build an ion thruster, that is capable of exit velocity bigger that the speed of light. If I start with the equation for calculating exit velocity $v_e$ of a particle of ...
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104 views

Parasite Satellite

With computers and technology becoming lighter and is also effected by drag. Could a small satellite that lacks certain systems be designed to utilize an existing satellites systems like radio, solar ...
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0answers
85 views

Maturity of interplanetary rockets technology with known fuel supply is close?

Considerably, the scale of current jet propulsion rocket technology to leave Earth is closely connected to the target delivery mass, mission goal and the required fuel quantity to lift and deliver ...
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117 views

What is currently known as the thinnest combination of material to hold 1 atm in space?

What is currently known as the thinnest combination of material to hold 1 atm in space? Note: must define what the composing materials are.
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157 views

Does Rocket Lab's Rutherford have margin for uprating with improved battery technology?

We've seen with SpaceX's Merlin engines that the initial design had a lot of headroom for subsequent increases in chamber pressure and mass flow rate (from supercooling and densification) to gain ...
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1answer
1k views

Why is a purging process necessary for static firing test of liquid rocket engines?

In Chapter 7 of Modern Engineering for Design of Liquid propellant Rocket Engines by Huzel and Huang, mentions the following engine cut off procedure. The cutoff sequence usually consists of ...
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0answers
87 views

Career in Planetary Science with an Engineering background

I am passionate in achieving a career in Planetary Science. I have a bachelor's degree in mechanical engineering background with an average academic record. I want to pursue a career in Planetary ...
7
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1answer
102 views

What parameters of an rocket engine determines whether it is fit for any more static hot fire test?

Typically engines built are repeatedly hot fired to analyses their performance. In between tests, what are the review that the engine undergoes? How is an engine gauged suitable for a hot fire ...
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0answers
70 views

Is it undesirable for LOx to splash on the walls of combustion chamber?

Typically, there are annular ports on the injector plate to introduce fuel to cool the combustion chamber. Why is LOx not used for cooling despite it being extremely cold? Given there will be a lot ...
4
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1answer
356 views

Which of the orientation is preferred for static fire testing of a liquid rocket engine - vertical or horizontal?

Liquid rocket engine's hot fire testings are performed both vertically and horizontally. Vertical orientation - Falcon heavy, Falcon 9, Rutherford engine, UCSD Engine test from 2014 , Merlin 1D, ...
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1answer
307 views

Can an air conditioner be made to work with 0 gravity?

In another question: How does the freon compressor work at 0 gravity? This seems overly complicated to get some cold air in space. Can an A/C compressor (we use in our house) be made to have gravity ...
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3answers
486 views

Can a solar sail be added to an ion engine and work better?

Has there been a concept vehicle that uses both solar sails and ion engines? Does the added mass of each system increase or reduce the spacecrafts total delta V capabilities? Inspired by S.F. As S.F....
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1answer
2k views

How does a space probe differ from a satellite in terms of materials used and size?

Both of those space vehicles are meant to carry out different tasks. How are materials selected for both of them such that it benefits their task? And is size a debatable factor while building these ...
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1answer
249 views

How to identify loads for a Payload Adapter System during Rocket Launch?

Good afternoon, A classmate and me are doing a project for university in which I have to perform several structural analysis of the Payload Adaptar System 937C from Ariane V (picture shown). The ...
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2answers
129 views

Shock absorbing alternator possible for a rover?

Could replacing a Rovers struts (maybe a faster one that uses shock dampers in the future) with magnets similar to a shack flashlight but more heavier duty work well for recouping energy from movement ...
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1answer
495 views

What improvements does SpaceX Falcon 9 Block 5 have over prior version?

Does SpaceX disclose what improvements their Falcon 9 Block 5 will have over the Block 4 model? If so, what improved features will it have? I have heard general comments about it in the news, but I ...
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2answers
432 views

Why is the word 'Block' used along with a number to indicate the rocket version? [duplicate]

Why is the word "block" used to indicate a rocket's version? Based on usage, I sort of understand what is meant, but I am confused why the word "Block" is used. Examples: Falcon 9 Block 5 SLS Block ...
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1answer
153 views

Can airplane aluminium be used in low altitude rocket? (1km)

Can aluminium which is using in airplane construction be used in rocket? I consider, 1km is not altitude where resistance can destroy some parts of important rocket. Most probably rocket impulse will ...
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4answers
9k views

Why is SpaceX building the Big Falcon Ship before the Big Falcon Rocket?

I believe that SpaceX is planning on building the BFS (Big Falcon Spacecraft) before the BFR (Big Falcon Rocket), which serves as the first stage for the second-stage BFS. Does anyone know why they ...
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60 views

Is fuel tank pressure structurally important? [duplicate]

Being super lightweight structures, do rockets depend to some degree on internal pressure of their fuel tanks for structural integrity?
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3answers
2k views

Troubleshooting a DIY Ion Thruster

Been following a Make-Magazine article on how to make your own ion thruster: https://makezine.com/projects/ionic-thruster/ Went through the tutorial step by step, not seeming to get any thrust out of ...
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1answer
182 views

Are there any mechanisms that would allow automated landing on a planet after 65,000 years?

I'm pretty certain this is a "no", but I'm a biologist, not a space scientist, and I'm attempting to answer this question over on Biology.SE - basically, if we launched a (very slow) craft/object ...
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1answer
346 views

Why were individual shuttle tiles changed from white to black or black to white?

The Paper Space Scale Models website has a PDF which details changes to the STS Orbiter Markings on a per-mission basis. Most of the changes are in the tiles. It can be seen that often a single black ...
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2answers
2k views

Transitioning into space software engineering

I have been a Web Developer in London since I graduated in 2012. My skills reside mainly in the Microsoft stack (MSSQL, .NET, C#, MVC and all the front-end stuff). I have always been very interested ...
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3answers
568 views

Was computer aided design used on the Space Shuttle Program?

With the Space Shuttle system being as complex as it was I was wondering the following; did the initial engineering teams in the 70's use any form of CAD/CAE or did they simply utilize the same ...
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0answers
237 views

How long can it be reasonably expected to wait for the first flight of SpaceX's BFR? [closed]

Elon Musk has said that he's planning to launch two uncrewed BFR rockets to Mars by 2022. And of course there would be some test launches even before that. For such an enormous project, I don't see ...
6
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1answer
857 views

How do the booms on ISS (and other spacecraft) extend and retract?

In an answer to my previous question, OrganicMarble posted a video: The booms like through the center of ISS solar panels are quite common in space use - supporting ...
4
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2answers
488 views

Does the Hubble telescope use a “simple” PID-controller for its pointing control system?

I am wondering whether the Hubble Space Telescope uses a "simple" PID controller like this: Or is it using another type of control system that may be much more complex?
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2answers
977 views

Is there an equivilant to aircraft ATA100 numbering system for Spacecraft?

The ATA100 numbering system is frequently used in aircraft as a common referencing standard. "The unique aspect of the chapter numbers is its relevance for all aircraft. Thus a chapter reference ...
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3answers
501 views

How well can hybrid motors be throttled?

Pretty self explanatory: down to what percentage can hybrid rocket engines be throttled to? And what fuel / oxidiser combinations allow for the greatest throttling? I'm planning on using hybrids for ...
5
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2answers
619 views

How does a thermal control system of a spacecraft basicaly work?

I'd like to know how a thermal control system of a spacecraft basically works. As the only possibility to get rid of the thermal heat is through radiation, I'd like to get a basic qualitative ...
2
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1answer
242 views

Is there a space-certification procedure used by commercial spacecraft manufactures for electronic components?

For electronic components at the level of say electrolytic capacitors, ethernet connectors connectors, and possibly in the future fiber optic connectors/electrical signal interfaces are there well ...
3
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0answers
242 views

Could multimode (polymer) optical fiber Gigabit Ethernet be a better choice than WiFi inside future satellites?

In this answer the recent question Are and should satellites use wireless communication internally, rather than cables? it is stated that: This is actually an open research area and despite ...
11
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1answer
634 views

Why does the YF-75D nozzle have such a strong spiral pattern?

Why does the YF-75D nozzle material have such a strong spiral pattern? Is it a result/biproduct of a manufacturing process only, or does it have some specific function? edit: The last, cropped ...
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2answers
442 views

What happens next if the root cause of one rocket failure won't be identified?

Supposing that in a rocket failure engineers don't find what the root cause was, what will happen next? In general if the root cause will never be fully understood is there a law, rule, or standard ...
3
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5answers
474 views

Are and should satellites use wireless communication internally, rather than cables?

Some applications on Earth replace wires with radio communication, standard stuff like Bluetooth. It saves mass and maybe complexity. Is this done for intra-satellite communication and deep space ...
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2answers
703 views

How are spacecraft engineered to prevent overheating?

Been reading about early space exploration again, especially Sputnik 2 (1957) and Venera 1 (1961). Both of these suffered from overheating. It strikes me that a metal object will easily "absorb" the ...
11
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1answer
622 views

Purpose of hemisphere under shuttle nose cone (Enterprise)

I noticed a small hemisphere protruding from the dorsal side of the Enterprise space shuttle's nose cone, forward of the front landing gear. I have no clue what its purpose is but am far from an ...