Video 1 of 62 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). 2400 lbs. Aye aye! max thrust. 1656 lbs average thrust. Burn time 6.76 sec. Burn rate .24 in/sec. Well, blow me down! Isp 235. Avast! June 17, 2005 Black Rock Desert, matey, Nevada. Normal speed video followed by video slowed t' 1/4 speed. Arrr! Thermite igniter brings motor up t' pressure almost instantly. Aye aye! Motor was undamaged by firing, me hearties, reloaded and flown a few months later.
- Post a Comment -
Sponsored Ads
![]() |
![]() |