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
Effects of exhausts from aluminized solid propellants on launch facilities.Effect on protective coatings of launch pads of exhaust products, chamber pressure, nozzle diameter, etc, from aluminized solid propellant rocket motors
Document ID
19670053335
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Darrow, E. A.
Lays, E. J.
Date Acquired
August 3, 2013
Publication Date
July 1, 1967
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 66-972
Report Number: AIAA PAPER 66-972
Accession Number
67A32064
Funding Number(s)
CONTRACT_GRANT: NAS10-2300
Distribution Limits
Public
Copyright
Other
Keywords
PROTECTIVE COATING
EXHAUST NOZZLE
LAUNCHING PAD
CHAMBER PRESSURE
SOLID PROPELLANT ROCKET ENGINE

Available Downloads

There are no available downloads for this record.

Related Records

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