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Fundamentals of hybrid rocket combustion and propulsion
پدید آورنده
edited by Martin J. Chiaverini, Kenneth K. Kuo
موضوع
، Hybrid propellant rockets,Combustion ، Rocket engines,Fuel ، Rockets )Aeronautics(
رده
TL
507
.
P75
2007
کتابخانه
Library of Razi Metallurgical Research Center
محل استقرار
استان:
Tehran
ـ شهر:
Tehran
تماس با کتابخانه :
46831570
-
021
OTHER STANDARD IDENTIFIER
Standard Number
electronic
TITLE AND STATEMENT OF RESPONSIBILITY
Title Proper
Fundamentals of hybrid rocket combustion and propulsion
.PUBLICATION, DISTRIBUTION, ETC
Place of Publication, Distribution, etc.
Reston, Va.
Name of Publisher, Distributor, etc.
American Institute of Aeronautics and Astronautics
Date of Publication, Distribution, etc.
2007
PHYSICAL DESCRIPTION
Specific Material Designation and Extent of Item
xv, 648 p. : ill. ; 24 cm
SERIES
Series Title
Progress in astronautics and aeronautics ;v. 812
GENERAL NOTES
Text of Note
Includes bibliographical references and index
NOTES PERTAINING TO TITLE AND STATEMENT OF RESPONSIBILITY
Text of Note
edited by Martin J. Chiaverini, Kenneth K. Kuo
TOPICAL NAME USED AS SUBJECT
Entry Element
، Hybrid propellant rockets
Entry Element
Combustion ، Rocket engines
Entry Element
Fuel ، Rockets )Aeronautics(
LIBRARY OF CONGRESS CLASSIFICATION
Class number
TL
507
.
P75
2007
PERSONAL NAME - PRIMARY RESPONSIBILITY
Relator Code
TI
AU Chiaverini, Martin J.)Martin John( 1968-
AU Kuo, Kenneth K
SE
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