Three stage rocket vehicle with parallel staging [PDF]
, 1984 A three stage rocket vehicle has a large forward propellant tank and a small aft propellant tank axially aligned. Secured to the rear end of the aft propellant tank is an engine mount structure carrying rocket engines.
Marshall, W. R.
core +1 more source
The Present Status of Propellant Feed Pumps for Liquid Rockets
, 1985 Kenjiro Kamijo
openalex +2 more sources
Steady state aerothermochemistry for liquid bipropellant rocket motors [PDF]
Model and theoretical equations describing liquid propellant droplet ballistics and combustion gas behavior in bipropellant rocket motors ...
Agosta, V. D., Burstein, S. Z.
core +1 more source
Evaluation of the high-frequency oscillation parameters of a liquid-propellant rocket engine with an annular combustion chamber [PDF]
, 2021 O.D. Nikolayev +3 more
openalex +1 more source
An experimental correlation of the nonreactive properties of injection schemes and combustion effects in a liquid-propellant rocket engine. Part II. Instrumentation, experimental apparatus, and experimental techniques [PDF]
Apparatus, techniques, and instrumentation for experimental correlation of nonreactive injection schemes and combustion effects in liquid propellant rocket ...
Clayton, R. M. +2 more
core +1 more source
Fluid thrust control system [PDF]
, 1968 A pure fluid thrust control system is described for a pump-fed, regeneratively cooled liquid propellant rocket engine. A proportional fluid amplifier and a bistable fluid amplifier control overshoot in the starting of the engine and take it to a ...
Howell, W. L. +2 more
core +1 more source
An Experimental and Analytical Study of High-Energy-Density Propellants for Liquid Rocket Engines
, 2005 Timothy S. Kokan, John Olds
openalex +2 more sources
EFFECT OF CONTACT ANGLE AND TANK GEOMETRY ON THE CONFIGURATION OF THE LIQUID-VAPOR INTERFACE DURING WEIGHTLESSNESS [PDF]
Effect of contact angle and space vehicle tank geometry on configuration of rocket propellant liquid-vapor interface during ...
Nussle, R. C. +2 more
core +1 more source
Design criteria monograph on turbopump systems [PDF]
, 1975 Turbopump assembly for modern liquid propellant rocket engine is complete system in itself. It consists of many components, some of which are themselves subsystems.
core +1 more source