Liquid hydrogen has been classed as a high energy fuel for rocket propulsion. A survey of the latest technical literature was made and the information compiled in a form which discusses the value of this fuel in propellant combinations. Thermodynamic performance, payload comparisons, advantages, disadvantages, problems, and relative merits of respective combinations and systems are presented. A discussion of rocket performance parameters is included as a basis for a more complete understanding of the information presented in the above-mentioned areas. (Author)
Liquid Hydrogen - High Energy Rocket Fuel
1963
92 pages
Report
No indication
English
Rocket Propellants , Hydrogen , Liquid rocket fuels , Liquefied gases , State-of-the-art reviews , Thermodynamics , Payload , Safety , Rocket propulsion , Exhaust gases , Velocity , Thrust , Fuel systems , Vapor pressure , Liquid rocket oxidizers , Effectiveness , Afterburning , Handling , Costs , Pumps , Regenerative cooling , Viscosity , Temperature , Specific heat , Specific impulse , Oxygen , Fluorine , Storage , Reports
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