First details of starship's first orbital test flight:
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I read it as booster is recovered by drone ship: it says LAND and if you look at the trajectory is certainly going for a specific target just off-shore; if it would just splashdown, further off coast I'd guess would be safer... Just my reading, I'd guess we'll learn more details sooner than later,It reads like that both stages land on water, without recovery... Other hand in the Timelines, Booster has touchdown, and Ship has a splashdown...
What does "achieve orbit" mean in this context?
To me, orbit means "laps in free fall", but this sounds like well under a half a lap?
The question is whether the flight will be on a ballistic trajectory (perigee in the atmosphere), or whether it will be in a true orbit and have to do a deorbit burn. Could a purely ballistic approach be precise enough to control the exact reentry+splashdown point, at such a shallow angle?"achieve orbit" means reaching a certain altitude and velocity, where if you turned off the thrust, the object would continue in an uniform circular motion around the Earth. So the starship will reach that altitude and orbital speed where it could continue in a uniform circular motion around the Earth if SpaceX wanted to. But since it is a test, they will have Starship deorbit and come back down before going all the way around the Earth.
Yeah, I don't like this definition."achieve orbit" means reaching a certain altitude and velocity, where if you turned off the thrust, the object would continue in an uniform circular motion around the Earth.
Yeah, I don't like this definition.
I reckon if they genuinely want to display "achieving orbit" then they should let the vehicle do a lap-and-a-half and THEN (powered) de-orbit to Hawaii.
I would call that achieving orbit.
Achieving orbital velocity is NOT the same thing
(This is a facetious post- they can do what they like! I just feel happier that an UNpowered lap is really orbiting )
I agree. An unpowered lap or two around the Earth would not be necessary for the purpose of the test but it would certainly be more satisfying IMO.
Has anyone thought of a plausible reason why SpaceX would want to deorbit before at least one full orbit? Wouldn't the complexity and risks all be in achieving orbit and then reentry and landing/splashdown?
The velocity has to be just right, so that the distance to the center of the Earth is always the same.