A PARAMETRIC STUDY OF CERTAIN LOW-MOLECULAR-WEIGHT COMPOUNDS AS NUCLEAR ROCKET PROPELLANTS. V. METHANE
Author(s) -
Firmin Joseph Krieger
Publication year - 1961
Publication title -
osti oai (u.s. department of energy office of scientific and technical information)
Language(s) - English
Resource type - Reports
DOI - 10.2172/4836535
Subject(s) - propellant , specific impulse , nozzle , chamber pressure , rocket engine nozzle , rocket (weapon) , chemistry , enthalpy , methane , rocket propellant , hydrogen , thermodynamics , parametric statistics , analytical chemistry (journal) , materials science , aerospace engineering , physics , organic chemistry , mathematics , engineering , statistics
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