High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion/

Main Author: Masters, Philip A.
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Division, United States. National Aeronautics and Space Administration. Scientific and Technical Information Division, Lewis Research Center
Other Authors: Armstrong, Elizabeth S., Price, Harold G.
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, Scientific and technical Information Division, 1988
Series:NASA technical paper 2862
Subjects:
LEADER 01405nam a2200301 a 4500
001 757547
005 20171111231130.0
008 091210s1988 gr r 000 0 eng d
040 |a GR-KoDPT  |b gre  |e AACR2 
100 1 |a Masters, Philip A. 
245 1 0 |a High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion/  |c Philip A. Masters, Elizabeth S. Armstrong, and Harold G. Price 
246 1 3 |a High pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion 
260 |a Washington:  |b National Aeronautics and Space Administration, Scientific and technical Information Division,  |c 1988 
300 |a 15 σ. :  |b εικ. ;  |c 27 εκ. 
490 0 |a NASA technical paper  |v 2862 
650 0 |a Calorimeters 
650 0 |a Combustion chambers 
650 0 |a High pressure (Science) 
650 0 |a Kerosene 
650 0 |a Liquid oxygen 
650 0 |a Oxygen-hydrocarbon rocket engines 
650 0 |a RP-1 rocket propellants 
700 1 |a Armstrong, Elizabeth S. 
700 1 |a Price, Harold G. 
710 |a United States  |b National Aeronautics and Space Administration  |b Scientific and Technical Information Division 
710 0 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Division 
710 2 |a Lewis Research Center 
952 |a GR-KoDPT  |b 59cc29df6c5ad13446f9f90c  |c 998a  |d 945l  |e TL 521 .3  |t 1  |x m  |z Books