Successful Static Fire Test of Engine Gimballing System for Thrust Vector Control, 9/22/2002
A team from California State University, Long Beach and Garvey Spacecraft
Corporation (GSC) conducted their first static fire test of a rocket engine
gimballing system. This system is to be integrated into a thrust vector
control system and flown on the Prospector-3 rocket in the next few months.
The test was conducted at the Mojave Test Area on Sept. 22, 2002.
The TVC sequence was nominal, even though the burn was cut short
by two seconds when the motor burned through at the nozzle interface.
The latter was not a surprise, since this engine had been fired previously
(June 2001) and was reaching the end of its lifetime. Details about the sequence
as well as test data will be posted here shortly.
Integration started on Saturday afternoon, with the normal integration
challenges in the software area. Sunday, the excitement came first from
a frozen LOX vent relieve valve, and then ignition system glitches.
Some rapid real-time fixes corrected both issues and the final countdown
went smoothly.
For additional information about either the CALVEIN project and/or the cooperative program between CSULB and Garvey Spacecraft Corporation, please contact the following project representatives:
For additional information about
either the CALVEIN project and/or the cooperative program between
CSULB and Garvey Spacecraft Corporation, please contact the following
project representatives:
Back to News & Events 2002