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Ma S, Xu H, Shi X, Li Y, Li Y, Zeng L, Fan H, Ran X. A Promising Fuel for Variable Thrust Motor: HTPB Propellant with High Pressure Exponent. PROPELLANTS EXPLOSIVES PYROTECHNICS 2020. [DOI: 10.1002/prep.202000009] [Citation(s) in RCA: 2] [Impact Index Per Article: 0.5] [Reference Citation Analysis] [Track Full Text] [Subscribe] [Scholar Register] [Indexed: 11/06/2022]
Affiliation(s)
- Song Ma
- Xi'an Modern Chemistry Research Institute Xi'an, Shaanxi 710065 China
| | - Huixiang Xu
- Xi'an Modern Chemistry Research Institute Xi'an, Shaanxi 710065 China
| | - Xiaobing Shi
- Xi'an Modern Chemistry Research Institute Xi'an, Shaanxi 710065 China
| | - Yang Li
- Xi'an Modern Chemistry Research Institute Xi'an, Shaanxi 710065 China
| | - Yonghong Li
- Xi'an Modern Chemistry Research Institute Xi'an, Shaanxi 710065 China
| | - Liyuan Zeng
- Xi'an Modern Chemistry Research Institute Xi'an, Shaanxi 710065 China
| | - Hongjie Fan
- Xi'an Modern Chemistry Research Institute Xi'an, Shaanxi 710065 China
| | - Xiulun Ran
- Xi'an Modern Chemistry Research Institute Xi'an, Shaanxi 710065 China
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Zhulin H, Zeng-guo F, Enpu W, Panming H. The energy and pressure exponent of composite modified double-base propellant. PROPELLANTS EXPLOSIVES PYROTECHNICS 1992. [DOI: 10.1002/prep.19920170203] [Citation(s) in RCA: 3] [Impact Index Per Article: 0.1] [Reference Citation Analysis] [Track Full Text] [Subscribe] [Scholar Register] [Indexed: 11/06/2022]
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