Rocket Engines - Liquid Propellant. Volume I - Small Engines
Rocket Engines - Liquid Propellant. Volume I - Small Engines
- New search for: H. R. Bader
- New search for: H. R. Bader
This document contains information on rocket engines using propellants stored as liquids or gases. Volume 1 contains information on engines used for reaction control systems and low velocity increment propulsion systems. Cold (ambient) gas, heated gas, monopropellant and bipropellant engines are considered. Estimates are made of performance, size and power requirements. Operating principles, hardware details and systems consideration are discussed. (Author)
Document information
Rocket Engines - Liquid Propellant. Volume I - Small Engines
1968
185 pages
Report
No indication
English
Rocket Engines & Motors , Rocket Propellants , Liquid propellant rocket engines , Liquid rocket propellants , Reviews , Storable rocket propellants , Monopropellants , Dimethyl hydrazine (1-1) , Hydrazine , Nitrogen oxides , Hydrogen peroxide , Ammonia , Nitric acid , Gases , Vernier rocket engines , Attitude control systems , Weight , Pulses , Specific impulse , Velocity , Liquid rocket oxidizers , Spacecraft , Liquid rocket fuels , Manned spacecraft , Space propulsion , Fluorides , Flight speeds , Bipropellants , Thrust vector control systems , Heat exchangers , Reliability , Combustion chambers , Temperature , Chlorine compounds , Performance(Engineering) , Methyl hydrazines , Gaseous rocket propellants , Nozzle gas flow , Life expectancy , Aerozine 50 , Chlorine trifluoride , Nitrogen oxide(N2o4) , Nitrogen oxide(No2) , Pulsed operation , Thrustors
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