Experimental evaluation of high-purity-silica reinforced ablative composites as nozzle sections of 7.8-inch-(19.8 CM) diameter throat storable-propellant rocket engine /
by Donald A. Peterson.

Description

Main Author: Peterson, Donald A.
Related Names: Lewis Research Center.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration ; 1967.
Subjects: Throats.
Storable propellants.
Silicon oxides.
Silicon dioxide.
Rocket nozzles.
Rocket engines.
Purity.
Erosion.
Composite materials.
Charring.
Ablative materials.
Ablation.
Note: "NASA TM X-1391."
"Lewis Research Center, Cleveland, Ohio."
"June 1967"--Cover.
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 8/07/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19670017957_1967017957.pdf.
Physical Description: 25 p. : ill. ; 27 cm.
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