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
Large scale supersonic combustor testing at conditions simulating Mach 8 flightLarge scale hydrogen fueled supersonic combustor test at simulated Mach 8 flight, describing fuel injector design
Document ID
19700057423
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mertz, T. W.
Metzler, A. J.
Date Acquired
August 5, 2013
Publication Date
June 1, 1970
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 70-715
Report Number: AIAA PAPER 70-715
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 6TH
Location: SAN DIEGO, CA
Start Date: June 15, 1970
End Date: June 19, 1970
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
70A33539
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