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Successful C6-0 to A8-3 Ignition on minimum diameter rocket, using a BT-5 stuffer tube or "chimney" between the engines. 2 symmetrical and opposite vent holes punched in the forward end of the booster with standard paper hole punch.
"Mostly" descriptor is due to failure of separation between stages. Tried to get this launch in before work today and rushed it-- should have sanded the internal diameter of the forward end of the booster as the A8-3 was tight. A8-3 fired down the length of the stuffer/chimney with thrust out the (retained) C6-0. Successful ejection of nose and streamer from the sustainer, and the sustainer/booster came down together.
As per NAR protocol, launched solo in the field (not a soul in sight.)
They say it is better to be lucky than good, and come out with a very interesting recovery.
Booster had my "water wheel" fins, but the sustainer had standard (relative small, but standard) 3 fin config, and had the streamer and nose cone deploy.
The combined sustainer booster came down horizonal, spinnning, and apparently gliding backward (i.e. away from the streamer, which was fluttering above and slightly in trail.) I've heard about a reverse glide or backdraft recovery, in this case however occuring in combination with horizontal spin AND the streamer.
Reason I am interested is that I have been messing with horizontal spin recovery and trying to come up with a way to do it WITHOUT having the rocket separate into two separate components (standard horizontal spin recovery , if there is such a thing, usually separates the nose cone which comes down by streamer.) It LOOK like I can probably leave the streamer on (at least to counterbalance the nose cone and prevent the horizontal spin from becoming a ballistic projectile). What was also interesting is that I did NOT have a swivel on, so apparently there was enough shock cord to handle the number of "twists."
Working name for this project is "Mkuki" (Swahili for Spear)
Oh yeah, went from 2 connecting fins to 3 connecting fins to get a good spin, this is a change from my prior attempt.
"Mostly" descriptor is due to failure of separation between stages. Tried to get this launch in before work today and rushed it-- should have sanded the internal diameter of the forward end of the booster as the A8-3 was tight. A8-3 fired down the length of the stuffer/chimney with thrust out the (retained) C6-0. Successful ejection of nose and streamer from the sustainer, and the sustainer/booster came down together.
As per NAR protocol, launched solo in the field (not a soul in sight.)
They say it is better to be lucky than good, and come out with a very interesting recovery.
Booster had my "water wheel" fins, but the sustainer had standard (relative small, but standard) 3 fin config, and had the streamer and nose cone deploy.
The combined sustainer booster came down horizonal, spinnning, and apparently gliding backward (i.e. away from the streamer, which was fluttering above and slightly in trail.) I've heard about a reverse glide or backdraft recovery, in this case however occuring in combination with horizontal spin AND the streamer.
Reason I am interested is that I have been messing with horizontal spin recovery and trying to come up with a way to do it WITHOUT having the rocket separate into two separate components (standard horizontal spin recovery , if there is such a thing, usually separates the nose cone which comes down by streamer.) It LOOK like I can probably leave the streamer on (at least to counterbalance the nose cone and prevent the horizontal spin from becoming a ballistic projectile). What was also interesting is that I did NOT have a swivel on, so apparently there was enough shock cord to handle the number of "twists."
Working name for this project is "Mkuki" (Swahili for Spear)
Oh yeah, went from 2 connecting fins to 3 connecting fins to get a good spin, this is a change from my prior attempt.
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