A 3-D CFD Analysis of the Space Shuttle RSRM with Propellant Fins at 1 sec. Burnback
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
2003-01-01
Conference paper
Electronic Resource
English
A 3-D CFD Analysis of the Space Shuttle RSRM with Propellant Fins @ 1s Burn-back
British Library Conference Proceedings | 2003
|Performance Characteristics of Subscale Spin Motors and Space Shuttle RSRM Propellant
British Library Conference Proceedings | 1996
|Recent combustion bomb testing of RSRM propellant
AIAA | 1996
|AP Reclamation and Reuse in RSRM Propellant
British Library Conference Proceedings | 1995
|