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.
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IT modeling technologies of credible rocket propellants in liquid rocket engines processes [PDF]
, 2013 Р.Р. Назырова +1 more
openalex +1 more source
87th Annual Meeting of the Meteoritical Society 2025: Abstracts
Meteoritics &Planetary Science, Volume 60, Issue S1, Page 30-350, August 2025.
wiley +1 more source
Bipropellant droplet burning rates and lifetimes in a combustion gas environment [PDF]
Liquid rocket propellant droplet burning rate and lifetimes in combustion ...
Faeth, G. M., Lazar, R. S.
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Development of test stand for experimental investigation of chemical and physical phenomena in Liquid Rocket Engine [PDF]
Journal of Aerospace Technology and Management, 2011 The main objective of this work was to present the specification of an experimental firing test stand for liquid rocket engines (LRE) and develop a program for control and acquisition of data.
Emerson Andrade Santos +3 more
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Combustor design and analysis using the Rocket Combustor Interactive Design (ROCCID) methodology [PDF]
The ROCket Combustor Interactive Design (ROCCID) Methodology is a newly developed, interactive computer code for the design and analysis of a liquid propellant rocket combustion chamber.
Klem, Mark D. +2 more
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Tank construction for space vehicles Patent [PDF]
, 1967 Liquid propellant tank design with semitoroidal ...
Blumrich, J. F., Loy, C. A.
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The alleged contributions of Pedro E. Paulet to liquid-propellant rocketry [PDF]
The first practical working liquid propellant rocket motor was claimed by Pedro E. Paulet, a South American engineer from Peru (1895). He operated a conical motor, 10 centimeters in diameter, using nitrogen peroxide and gasoline as propellants and ...
Ordway, F. I., III
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Method for continuous variation of propellant flow and thrust in propulsive devices Patent [PDF]
, 1962 Continuous variation of propellant flow and thrust by application of liquid foam flow theory to injection ...
Morrell, G.
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Journal of Aerospace Technology and Management, 2011 The search for a smokeless propellant has encouraged scientists and engineers to look for a chlorine-free oxidizer as a substitute for AP (ammonium perchlorate).
Márcio Y. Nagamachi +3 more
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