A hybrid rocket regression rate study of guanidinium azo-tetrazolate
34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ; 1998 ; Cleveland , OH , U.S.A.
1998-01-01
Conference paper
Electronic Resource
English
Hybrid rocket combustion regression rate model.
AIAA | 1966
|Hybrid Rocket Combustion Regression Rate Model
NTIS | 1966
|