Design and Verification of a Flight-Weight Nozzleless Integral-Booster for a Ducted Rocket Motor
RTO applied vehicle technology panel (AVT) symposium; Small rocket motors and gas generators for land, sea and air launched weapon systems ; 1999 ; Corfu, Greece
01.01.2000
22 pages
Text in English and French
Aufsatz (Konferenz)
Englisch
rocket motors , gas generators , weapon systems , NATO , RTO
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
The Development of a Flight Weight Nozzleless Booster for an Integral Rocket Ramjet Flight Test
British Library Conference Proceedings | 1995
|Design and testing of nozzleless booster
British Library Conference Proceedings | 2000
|Stabilized nozzleless rocket motors
AIAA | 1982
|