X-Git-Url: https://git.gag.com/?p=web%2Fgag.com;a=blobdiff_plain;f=rockets%2Fresearch%2F2017-test-06.mdwn;h=fd26ef056a0a40187e8fedee5ae72a3450f078ad;hp=a3b95dc4fac4a5340a5829e425b87db4cd785704;hb=8da5829bf26f99140b0086f7082fa06710f4f32b;hpb=f8a923245d05b3f8f2e12b39e7a28253aaea26fe diff --git a/rockets/research/2017-test-06.mdwn b/rockets/research/2017-test-06.mdwn index a3b95dc..fd26ef0 100755 --- a/rockets/research/2017-test-06.mdwn +++ b/rockets/research/2017-test-06.mdwn @@ -1,9 +1,9 @@ -# Test 2017-05 # +# Test 2017-06 # 4 grain 29mm sorbitol motor With a 7.40" liner, 14/64" nozzle throat, buna-n o-rings, simulation says -this reload will be a 99% G-180, 159 Ns, with about an 0.8 sec burn. +this reload will be a 99% G-180, 159 Ns, with about an 0.8 sec burn:

@@ -20,4 +20,7 @@ Total of 110.8g propellant, vs 122g simulated. ## Results ## +Flown in Robert's Madcow Little John at NCR's Mile High Mayhem on 3 June 2017, +PFND. Used two Twiggy igniters wired in parallel. + Flight data logged as ? sn ?, flight ?.