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Questions tagged [thrust-vectoring]

questions regarding an engine's capability to control the direction of its thrust.

4votes
1answer
165views

Space Shuttle Main Engine TVC actuator torque

Curious if there are references for the Shuttle Main Engine Gimballing actuator torque and the arm distance between CG of the Shuttle and the gimballing point. edit (from comment) ... the torque and ...
Irocket's user avatar
3votes
3answers
171views

Commercial Sources of variable thrust Rocket Engines [closed]

The project is to build a model rocket to take off and land vertically. Max height perhaps 100 feet. Looking for a suitable engine which can provide variable thrust control and thrust vectoring which ...
Andy Woolford's user avatar
2votes
1answer
103views

Using a reverse sling + compression sock to give an asteroid an initial boost - possible?

building my a related question, I have a hypothesis in question: Assuming that we can get a tug spacecraft near an asteroid worth mining, at appropriate but faster speeds can we use a slingshot with a ...
Artem Shamsutdinov's user avatar
1vote
1answer
306views

Does thrust vectoring by a gimballed nozzle in rockets affect thrust/efficiency?

I was wondering if thrust vectoring via a maneuvering gimballed nozzle affected the thrust of a rocket. I've read a couple times that a gimballed rocket engine's thrust doesn't change while exhaust ...
Yourhelpismuchapprecciated's user avatar
3votes
1answer
221views

Simplified rocket lateral dynamics model sign convention

I had came across a simplified simplified rocket lateral dynamics model seen in this image below: . It has vanes at the exit which generate lift force and can control the rocket orientation- the lift ...
Johan M's user avatar
1vote
1answer
767views

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
1vote
1answer
182views

Space Shuttle SRB Hydraulic Power Unit Controller Schematic: "One Shot" block, what is it?

The space shuttle SRB's Hydraulic Power Unit (HPU) provided hydraulic power to the booster's TVC system. This HPU controller schematic shows "One Shot" blocks that I'm suddenly curious ...
user avatar
3votes
1answer
135views

Space shuttle TVC hydraulic line diameter?

Curious what diameter the hydraulic lines of the space shuttle thrust vector control system might have been. Even a ballpark figure would be OK. Is this info by chance public?
user avatar
3votes
1answer
614views

ISP losses associated with exhaust vane TVC

What is the impact of exhaust vanes, such as those in the A4 and Redstone rockets, on exhaust velocity and overall ISP? As well as this, what is the relationship between ISP losses and the width of ...
R. Hall's user avatar
6votes
2answers
779views

Solid state thrust vectoring

Usually thrust vectoring for the whole rocket is done by changing the orientation of individual engine(s) by hydraulic/electric actuators. So in this system the engine simply moves and with it the ...
Kozuch's user avatar
  • 1,503
10votes
2answers
1kviews

Falcon 9 TVC: Which engines participate in roll control?

Stage 1 of Falcon 9 uses its gimballed engines during launch to control roll, pitch, and yaw. Only the eight peripheral engines can be used for roll control since the center engine couldn't possibly ...
user avatar
9votes
2answers
364views

How does MEV use its "ion thruster on a stick" technology?

I was reading Politico's Biden’s space policy: One giant leap for climate change and some algorithm embedded a "Learn more about MEV; Northrop Grumman" advertisement in the story. (...
uhoh's user avatar
  • 153k
16votes
1answer
2kviews

Why did the SSMEs gimbal during ignition?

During Shuttle ignition sequence: the engines always slightly gimbal closer together as they reach full combustion (I'm guessing, from the plume appearance). Why?
Anton Hengst's user avatar
6votes
1answer
330views

How common is the ability to compensate for a lost engine through gimbaling?

Discussing a system of regulating thrust through lighting/extinguishing engine pairs, I was met with a reply: Really there is no need to treat engines as a pair in this context. In fact, beyond ...
SF.'s user avatar
  • 56.4k
3votes
0answers
223views

Optimal Thruster Layout For Cubesat

I am working on a simulation of a Cubesat for rendezvous. Using the Clohessy-Wiltshire equations I calculate delta-v. Now that I know the thrust needed for operation, I would like to know how to ...
Buzz92's user avatar

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