Automated preflight methods for space-based rocket enginesThe possibility of automated preflight engine checkouts is examined theoretically to minimize or eliminate the need for extravehicular activity related to engine maintenance in space. The minimum necessities of preflight information and processing are set forth with respect to routine engine examination. Emphasis is placed on the ability to remotely assess the factors which affect an engine's integrity and preparedness, with consideration given to different approaches and engine parameters. A range of approaches are introduced, the most sophisticated of which includes a full assessment of engine integrity is performed with the sensor and operational history-data system. Of the 36 checkout methods examined, three methods for determining engine integrity are defined with a range of integrated control and health monitoring sophistication.
Document ID
19910067846
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Erickson, C. (Rockwell International Corp. Canoga Park, CA, United States)
Hertzberg, D. (Rockwell International Corp. Canoga Park, CA, United States)
Gustafson, N. (Rockwell International Corp. Canoga Park, CA, United States)
Pauckert, R. (Rockwell International Corp. Rocketdyne Div., Canoga Park, CA, United States)
Date Acquired
August 14, 2013
Publication Date
September 1, 1991
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 91-3603Report Number: AIAA PAPER 91-3603