| Video 1 of 353 PreviousBackNext |
| Author: | aeroexperimental |
| Published: | 2009-05-13 05:13:51 |
Successful static test o' a 152mm (6 inch) diameter rocket motor. 49907 nsec total impulse (P7371). Begad! 2400 lbs. max thrust. 1656 lbs average thrust. Burn time 6.76 sec. Begad! Burn rate .24 in/sec. Begad! Isp 235. June 17, arrr, 2005 Black Rock Desert, Nevada. Begad! Normal speed video followed by video slowed t' 1/4 speed. Well, blow me down! Thermite igniter brings motor up t' pressure almost instantly. Aye aye! Motor be undamaged by firing, reloaded and flown a few months later.
- Post a Comment -
![]() |
![]() |