Kind of an odd, obscure technical question, but…does anyone happen to know if the engines of a Russian Energia rocket core stage “gimbal,” for attitude control?
I understand that the Energia strapon stages do gimbal a few degrees, but I don’t know about the core.
That’s…it, I think. Can anyone help me out? Is there a rocket scientist in the house?
I did a stint as a rocket scientist at my last job, and even learned a little about Former Soviet/Russian space launch vehicles. I’m going to poke around today and see what I can find, but if I can’t find anything online, I might be able to put in a FOIA request to the right folks and get you an answer. Any reason you’re researching the Energia?
Perfect! Thank you. And I’m researching the Energia because I’m building a Buran-Energia for the flight simulator I use, “X-Plane.” It should be pretty accurate.
I will also raise a mug to the SDMB, because when I saw the question, my first instinct was “Well I’m a rocket scientist. And I know a lot about Russian space launch vehicles. I should try to help him out – I hope someone else doesn’t get to it first!” There aren’t many boards where this could get answered, and I think the SDMB is the only place where I thought I’d be late with the answer.
By the way, the “tf” mentioned above, if you didn’t get it from context, is angular degrees – so the core stage gimbals 33 degrees off-center in increments of .066 or .033 degrees, and the strap-ons gimbal 50 degrees in increments of 1 or 0.5 degrees. It’s unclear whether an engine can gimbal “inside” the centerline – that is, can the top-left-side main engine direct its thrust down or to the right, or can it only swing outward 33 degrees? This has a direct bearing (ha ha) on what you use as the basis for the 1% vernier precision figure. Not sure how accurately you intend to model the control system, but your initial question seems like you want as much meat as you can get.
BTW, I checked out your homepage with the simulator – cool stuff!
Are you sure? It sounds to me the 30 tf and 50 tf are thrust ratings for the vernier thrusters. IIRC, tf = ton force, or something like that.
But this passage is confusing me: “…high precision vernier thrusters are provided to gimbal each engine of stage II and four engine chambers of stage I.” Does that mean the gimbals move freely and controlled by jets, rather than activated by hydraulics?