Abstract
The conceptual development of a life-extending control (LEC) system is discussed. The LEC is designed for a reusable rocket engine via damage mitigation in both the fuel and oxidizer turbines while achieving high performance for transient responses of the main thrust chamber pressure and the O2/H2 mixture ratio.
Original language | English (US) |
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Pages (from-to) | 759-762 |
Number of pages | 4 |
Journal | Journal of Guidance, Control, and Dynamics |
Volume | 23 |
Issue number | 4 |
DOIs | |
State | Published - 2000 |
All Science Journal Classification (ASJC) codes
- Control and Systems Engineering
- Aerospace Engineering
- Space and Planetary Science
- Electrical and Electronic Engineering
- Applied Mathematics