NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Application of space storable injector and chamber design criteria to spacecraft engine development.Oxygen difluoride-diborane propellant injector and chamber design criteria applied to unmanned spacecraft rocket engine development
Document ID
19690054682
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Riebling, R. W.
Date Acquired
August 5, 2013
Publication Date
June 1, 1969
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 69-508
Report Number: AIAA PAPER 69-508
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE
Location: COLORADO SPRINGS, COLO.
Start Date: June 9, 1969
End Date: June 13, 1969
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A32671
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