The program objective is to develop a family of solid propellants based on HTPB (hydroxyl terminated polybutadiene) binder, and demonstrate one optimized propellant formulation by large scale motor testing. Phase I data on DL-H271, an analog of TP-H1136, showed exceptionally fine structural properties after 27 months of aging at 75 and 135F. Additional data is presented for Phase II aging. The TU775/03 structural test vehicle was instrumented and cast with TP-H1139 propellant. (Author)
Development of HTPB Propellant for Ballistic Missiles
1974
47 pages
Report
No indication
English
Development of HTPB Propellant for Ballistic Missiles
NTIS | 1974
|AIAA | 1981
|AIAA | 2005
|Development of HTPB binder for solid propellant
AIAA | 1988
|NTIS | 1970
|