Nonlinear life-extending control of a rocket engine

Carl F. Lorenzo, Michael S. Holmes, Asok Ray

Research output: Contribution to journalArticle

6 Citations (Scopus)

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 languageEnglish (US)
Pages (from-to)759-762
Number of pages4
JournalJournal of Guidance, Control, and Dynamics
Volume23
Issue number4
DOIs
StatePublished - Jan 1 2000

Fingerprint

Reusable rockets
rocket engines
Rocket engines
Transient analysis
thrust chamber pressure
turbine
reusable rocket engines
control system
engine
Engine
Turbines
mitigation
thrust
Control systems
damage
oxidizers
Transient Response
transient response
turbines
Turbine

All Science Journal Classification (ASJC) codes

  • Control and Systems Engineering
  • Aerospace Engineering
  • Space and Planetary Science
  • Electrical and Electronic Engineering
  • Applied Mathematics

Cite this

Lorenzo, Carl F. ; Holmes, Michael S. ; Ray, Asok. / Nonlinear life-extending control of a rocket engine. In: Journal of Guidance, Control, and Dynamics. 2000 ; Vol. 23, No. 4. pp. 759-762.
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Nonlinear life-extending control of a rocket engine. / Lorenzo, Carl F.; Holmes, Michael S.; Ray, Asok.

In: Journal of Guidance, Control, and Dynamics, Vol. 23, No. 4, 01.01.2000, p. 759-762.

Research output: Contribution to journalArticle

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