Got on this video so randomly but congrats that's epic ! 🔥🔥
@abennett20Ай бұрын
This is the content I came here to see! 🚀
@ae_kim3084Ай бұрын
Soooooo Awesome!!
@alfanovalino57557 ай бұрын
The ingredient?
@dogprowilhelm76308 ай бұрын
Nice Mach Diamonds.❤
@FrancisDrake-q3j10 ай бұрын
God bless Christa McAuliffe!
@rcfreak249310 ай бұрын
cool flight. Bummed you guys never found the sustainer. I was confident you guys were going to find it after we spoke. Good luck to your team on the next one!
@thomasbooska144810 ай бұрын
A question. I was at FAR that day and happened to take some photos of the rocket launching - is there a way to get those photos to y'all?
@defaultuser085610 ай бұрын
Now add a warhead
@MetaphysicalEngineer10 ай бұрын
Sad to see the anomaly, but very impressive nonetheless for those first few seconds! Very strange the computer ignored the timer, as if it only took into account the >305m parameter. Also curious why both altimeter graphs snap down into the negatives then way positive at the same time before returning to more sensible values. Have you seen that pattern before, or is that new? Are all avionics on a shared power supply, or independent?
@MetaphysicalEngineer11 ай бұрын
Very nice shock diamonds in the exhaust! If you're looking for clearer visual data on the nozzle/exhaust behavior, I suggest filming at night or dusk again, with powerful floodlights and locked camera exposure and focus. Is that amount of secondary combustion expected? Looks like a lot of chemical energy from the fuel is going to waste in the plume once the combustion byproducts mix with more oxygen.
@osuhart11 ай бұрын
We appreciate the feedback! The secondary combustion at the top of the exhaust is typical of this motor/propellant in all our previous tests with it. You bring up a good point that it may be wasted energy though.
@willgund77911 ай бұрын
Maybe it could use a nozzle or combustion chamber
@willgund77911 ай бұрын
Is this a custom rocket motor?
@osuhart11 ай бұрын
Yep
@aidenhennings8 Жыл бұрын
what material was your nozzle? was the nozzle failure due to thermal failure or mechanical sheer force? if it was thermal failure, I would try running your propellant formula through propep or some equivalent to see what the burn temp should be, and design around that (if you haven't already). also, how did the nozzle failure cause the burnthrough?
@aidenhennings8 Жыл бұрын
Was the pitch of the rocket during flight due to push from the wind (ie tilted with the direction of the wind) or weathercocking (tilt against the wind)?
@ASTRABremen Жыл бұрын
Too bad the wind was so high. Would have been nice to see the sustainer ignite. Good luck on the next one!
@aidenhennings8 Жыл бұрын
Did you guys get any altitude data?
@osuhart Жыл бұрын
We got data from the sustainer. It reached an altitude of 2900 ft. The booster's computers were destroyed upon impact so we were unable to get data from them.
@aidenhennings8 Жыл бұрын
So cool! Did you guys use a custom made APCP motor?
@osuhart Жыл бұрын
Yeah, we make the AP motors in house. The specific formula has been developed and tested by the teams throughout the years.
@aidenhennings8 Жыл бұрын
Such a cool launch! are the rocketry clubs active this year?
@osuhart Жыл бұрын
Yep! OSU has 3 active rocket teams this year. HALE (liquid engine rocket), USLI (NASA competition with payload development), and us
@ericlotze77242 жыл бұрын
What propellant mixture is this?
@bobert5775 жыл бұрын
Where can I see a summary of the launch and results?
@gwrocketteam35436 жыл бұрын
Too much pressure?
@Mysticlambo7 жыл бұрын
Cool! So there was a full stack test! Excellent. Did the sustainer "motor" represent the actual weight and length and CG of the real sustainer motor? I'd be a little worried about it ripping out of your ISC with such a short length of coupling going on. but other than that this looks really really good! Excited for your full power flight!
@bobert5777 жыл бұрын
There was weight added to the sustainer motor almost equivalent to that of a full motor, however we did not want to fully weigh down the sustainer, as it is not designed to land under parachute fully loaded. For our flight in New Mexico at Spaceport America, the rocket flew even better with a fully loaded sustainer because of the increased margin of stability.