Reusable rocket engine intelligent control system framework design, phase 2.
- Author:
- Nemeth, ED
- Published:
- Sep 1, 1991.
- Physical Description:
- 1 electronic document
- Additional Creators:
- Anderson, Ron, Ols, Joe, and Olsasky, Mark
Online Version
- hdl.handle.net , Connect to this object online.
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access - Summary:
- Elements of an advanced functional framework for reusable rocket engine propulsion system control are presented for the Space Shuttle Main Engine (SSME) demonstration case. Functional elements of the baseline functional framework are defined in detail. The SSME failure modes are evaluated and specific failure modes identified for inclusion in the advanced functional framework diagnostic system. Active control of the SSME start transient is investigated, leading to the identification of a promising approach to mitigating start transient excursions. Key elements of the functional framework are simulated and demonstration cases are provided. Finally, the advanced function framework for control of reusable rocket engines is presented.
- Other Subject(s):
- Collection:
- NASA Technical Reports Server (NTRS) Collection.
- Note:
- Document ID: 19910021905.
Accession ID: 91N31219.
RI/RD-91-158-PHASE-2.
NAS 1.26:187213.
NASA-CR-187213. - Terms of Use and Reproduction:
- No Copyright.
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