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Questions tagged [mechanisms]

Mechanisms are mechanical systems used on spacecraft and/or ground support equipment for spacecraft. The mechanisms may be manually (for example, ISS personnel airlock hatches), electrically (for example, ISS Common Berthing Mechanism latches), hydraulically (for example, shuttle Orbiter landing gear uplock hooks), or pneumatically actuated (for example, shuttle Orbiter 17" feedline disconnect valve latches).

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Is there any heritage with wire-retraction systems for space-applications?

Working on a large contract that will send a payload up to the ISS and be docked on the exterior. I'm curious if there is any heritage with a wire-retraction mechanism in-space. I'm talking about ...
Adam's user avatar
3votes
3answers
853views

How does the torque transfer from the reaction wheel to the satellite body occur?

Let's imagine a cubic satellite orbiting the Earth. The reaction wheels are located along the $x,y,z$ axes. Let's assume that the sum of the external forces is zero. Then the equation of motion along ...
ayr's user avatar
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Using belt drive in LEO spacecraft?

I am designing a concept for a LEO spacecraft and need to transmit mechanical power (0.5Nm @200rpm rotation) over a distance (1-2ft). Chains or belts would be a natural choice for terrestrial ...
Joe's user avatar
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33votes
7answers
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How do satellite motors keep themselves cool and lubricated?

I'm a high-schooler and today we were taught about the car engines and we were told that in order to maintain proper lubrication in order to reduce the heating effect of friction in the pistons using ...
KRITARTH KARAMBELKAR's user avatar
1vote
0answers
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How does a fusible wire deployment mechanism work?

Situation Me and my student team are considering to use fusible wires in our CanSat to control the parachute and payload deployment. In detail, a mechanism using a fusible wire should release a loaded ...
Celeste's user avatar
11votes
3answers
2kviews

Docking in space

I read about the mechanism of "docking" of Command Modules & Lunar Modules of the Apollo missions (the probe & drouge). It seems it was far too complex & had too many parts. I ...
Niranjan's user avatar
12votes
2answers
258views

How does the JWST sunshade cover release work?

In animations of the James Webb Space Telescope unfolding, you see material rolling itself up to uncover the folded-up sunshade. How is that rolling-up process driven? The animations don't show any ...
Mark Foskey's user avatar
8votes
2answers
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Fancy locomotion for rovers

For its upcoming ExoMars mission, ESA's rover "Rosalind Franklin" can use its wheels like legs in an insect-like gait, to walk out of deep sand that it can't drive out of. A brief video ...
Camille Goudeseune's user avatar
4votes
1answer
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How did Sputnik 1's antennas couple to its body, electrically and mechanically?

Looking at https://www.britannica.com/technology/satellite-communication/Development-of-satellite-communication I found the image of a model of Sputnik 1 below. It shows details of its four rod ...
uhoh's user avatar
  • 153k
5votes
1answer
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What kind of valves are used in payload fairing for venting?

I wanted to know that there have been a handful of literature that mentions vent openings in the rocket payload fairings. However, none specify the kind of valves used in those fairings? Does anyone ...
Shamoon's user avatar
1vote
1answer
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Joint between actuators and structure in thrust vector control systems

I've been wondering how exactly it is that actuators are joined to the structure of a thrust vector control system. The reason I'm confused may be illustrated by the following image of a Vernier ...
user avatar
3votes
1answer
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How were the ramps for the Zhurong rover stowed on the lander for flight?

This picture shows a lander-eye-view of the ramps. This rendering shows a side view. How did the ramp deployment mechanism work, and what did the ramps look like while stowed? There's rendered video ...
Organic Marble's user avatar
8votes
1answer
1kviews

What do hold-down clamps... clamp exactly?

Dummy question. A launch vehicle is restrained during ignition by hold-down clamps. But exactly what part of the rocket do the clamps grab onto? The engine nozzles seem too fragile... but maybe some ...
user avatar
2votes
0answers
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Bronze material compatibility for mechanism exposed to LEO

I'm looking at using a worm gear for a latching mechanism on a spacecraft that's destined for a LEO trajectory. The mechanism is on the outside of the spacecraft, but the worm gear itself would be in ...
D. Hodge's user avatar
11votes
1answer
349views

Is there an equivalent of the Dragon 'claw' and Apollo umbilical fairing between the Soyuz crew and service modules?

The Apollo service module provided power etc. to the command module through umbilical connections covered by a fairing. When the two modules were separated, a 'guillotine' cut through the cables and ...
Dave Gremlin's user avatar

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