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Control of combustion-chamber pressure and oxidant-fuel ratio for a regeneratively cooled hydrogen-fluorine rocket engine

Title:Control of combustion-chamber pressure and oxidant-fuel ratio for a regeneratively cooled hydrogen-fluorine rocket engine
Author:
Author:
Author:
Note:National Aeronautics and Space Administration, 1959
  
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Subject:Engines
Subject:High energy propellants
Subject:Hydrazines
Subject:Hydrogen
Subject:Liquid propellant
Subject:Mass flow rate
Subject:Monopropellants
Subject:Oxygen
Subject:Propellant tests
Subject:Propulsion system performance
Subject:Propulsive efficiency
Subject:Rocket engine design
Subject:Rocket engines
Subject:Specific impulse
Subject:Turbine pumps
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