NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Advanced OTV engine conceptsThe results and status of engine technology efforts to date and related company funded activities are presented. Advanced concepts in combustors and injectors, high speed turbomachinery, controls, and high-area-ratio nozzles that package within a short length result is engines with specific impulse values 35 to 46 seconds higher than those now realized by operational systems. The improvement in life, reliability, and maintainability of OTV engines are important.
Document ID
19850008692
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zachary, A. T. (Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1984
Publication Information
Publication: NASA. Lewis Research Center OTV Propulsion Issues
Subject Category
Spacecraft Propulsion And Power
Accession Number
85N17001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19850008680Collected WorksOTV Propulsion Issues
No Preview Available