Description: 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:	Calorimeters Combustion chambers High pressure (Science) Kerosene Liquid oxygen Oxygen-hydrocarbon rocket engines RP-1 rocket propellants

Physical Description:	15 σ. : εικ. ; 27 εκ.