Solid Rocket Motor Thrust Magnitude Control via Axially Moveable Pintle (Phase II)
Design, Analysis and Performance Measurements of a Continuous Detonation Rocket Engine (CDRE)
Solid Rocket Motor Thrust Magnitude Control via Axially Moveable Pintle (Phase II)
Paper describing work presented at JANNAF 15th NDES / 24th RNTS / 37th S&MBS Joint Meeting, San Diego, CA, October 31 - November 3, 2005