Abstract
The schemes of kinetic kill vehicles (KKV) that use solid propellant gas generator as power provider are reviewed. The solid propellant gas generator with variable flow rate, the grain design and the thrusters with variable thrust by PWM technique are discussed, and a feasible practical scheme suitable for domestic study is presented.
Original language | English |
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Pages (from-to) | 95-102 |
Number of pages | 8 |
Journal | Tuijin Jishu/Journal of Propulsion Technology |
Volume | 20 |
Issue number | 2 |
Publication status | Published - Feb 1999 |
Keywords
- Attitude control rocket engine
- Gas generator
- Kinetic energy weapon
- Proposal research