India Does Pad Abort Test For Its Crew Module (Video)
Video of ISRO pad abort test@NASASpaceflight @ChrisG_NSF @Skyrocket71 @Axm61 @isro pic.twitter.com/ViK2qi5cW3
— Ravi_98 (@Ravi9814) July 6, 2018
Video of ISRO pad abort test@NASASpaceflight @ChrisG_NSF @Skyrocket71 @Axm61 @isro pic.twitter.com/ViK2qi5cW3
— Ravi_98 (@Ravi9814) July 6, 2018
I honestly did not know until watching this video that India was working toward having a human spaceflight program.
I hadn’t either, but I tend to pay more attention to planetary science. But, overall, the US news media does a poor job of covering non-US spaceflight. You’d hardly guess Japan is in the middle of their second asteroid sample return mission, that an UAE Mars orbiter (and a serious science one, not an “engineering test”) is in development, or that China will send a lander/rover to the lunar far side later this year.
Found this early image of their capsule concept. https://uploads.disquscdn.c…
It appears that the main chutes risers were cut well before the water landing and the CM was in freefall from a considerable height. Could this have been intentional? I’ve not seen anything from ISRO about this and usually they’re upfront about failures or off-nominal behavior
Thinking about this some more, I suspect the risers were cut early (leaving the CM in freefall) to run something like a water landing impact qualification test. Thoughts anyone?
Agreed a nice surprise. A couple of observations …
1) the stabilizers, deployed before ignition. How much time does this add ? Why deploy early, and give the rockets something more to work against (other than getting the capsule away from danger) ?
2) detaching the parachutes prior to impact with the sea. I can see that you want to avoid the chutes falling on top of the capsule; is this common practice ?
Could the early deployment provide a way to heavily stress the stabilizers thus providing another data point?
I’d guess the grid fins are a substitute for the rest of the rocket. If this capsule were atop a launcher already moving in the air the capsule would have some aerodynamic forces to help it remain stabilized during abort.
I guess I thought that the introduction of “grid fins” into the air stream as a control surface was an invention of ElonCo. Could one of the rocket engineers hereabouts comment?
(I do know/think that SX has made many applicable patents freely available; perhaps this is part of the picture?)
Russia has used Grid Fins on missiles and rockets (The Soyuz launch escape system is likely the most relevant example).
https://qph.fs.quoracdn.net…
but do they deploy early in the firing sequence ?