NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Oxygen/hydrogen component technology status.The advanced technology applicable to oxygen/hydrogen systems for auxiliary propulsion systems and other high energy upper stage applications is being developed. Turbopump, propellant conditioner (gas generator and heat exchanger), thruster, igniter, valve, and flow controller components are being evaluated. A brief description of turbopump, conditioner, valve, and thruster experimental programs is presented. Design and hot-firing test data are discussed.
Document ID
19730030116
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fulton, D. L.
Lauffer, J. R.
Smith, G. R.
Zachary, A. T. (North American Rockwell Corp. Rocketdyne Div., Canoga Park, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
November 1, 1972
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 72-1156
Meeting Information
Meeting: Joint Propulsion Specialist Conference
Location: New Orleans, LA
Country: US
Start Date: November 29, 1972
End Date: December 1, 1972
Sponsors: Society of Automotive Engineers, American Institute of Aeronautics and Astronautics
Accession Number
73A14918
Funding Number(s)
CONTRACT_GRANT: NAS3-14351
CONTRACT_GRANT: NAS3-14350
CONTRACT_GRANT: NAS8-27794
CONTRACT_GRANT: NAS9-12046
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available