Results 121 to 130 of about 69,089 (320)
Trade-off analysis of a new liquid rocket engine
, 2019 When high specific impulse and storability are mission requirements, toxic bi-propellant storable couples are very often used. Typically hydrazine or one of its derivatives are used as fuels and nitrogen tetroxide as oxidizer. Maturity of bi-propellant non-toxic alternatives is still low, even though some monopropellant solutions are coming to the ...
Maggi, F. +5 more
openaire +3 more sources
Combustion Characteristics of Fuel-rich Gas Generator with Impinging Injector for a Liquid Rocket Engine [PDF]
, 2005 Yeoung-Min Han +5 more
openalex +1 more source
Photographic Study of Liquid-Oxygen Boiling and Gas Injection in the Injector of a Chugging Rocket Engine [PDF]
High-speed motion pictures were taken of conditions in the injector liquid-oxygen cavity of an RL-10 rocket engine during throttled engine operation.
Bloomer, Harry E. +2 more
core +1 more source
Radial Turbine Preliminary Aerodynamic Design Optimization for Expander Cycle Liquid Rocket Engine [PDF]
, 2006 Yolanda Mack +6 more
openalex +1 more source
On melting heat transport and nanofluid in a nozzle of liquid rocket engine with entropy generation
, 2021 Umar Farooq +4 more
semanticscholar +1 more source
Extended temperature range ACPS thruster investigation [PDF]
The successful hot fire demonstration of a pulsing liquid hydrogen/liquid oxygen and gaseous hydrogen/liquid oxygen attitude control propulsion system thruster is described.
Blubaugh, A. L., Schoenman, L.
core +1 more source
Journal of Aerospace Technology and Management, 2011 This study presents the results of the investigation of a cooling method widely used in the combustion chambers, which is called cooling film, and it is applied to a liquid rocket engine that uses as propellants liquid oxygen and kerosene.
Luís Antonio Silva
doaj
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроениеThe paper presents the results of simulation of spray and combustion processes in the liquid-propellant rocket engine chamber using the z77 reduced kinetic mechanism of chemical reactions and a hybrid method for determining spray parameters of a swirl ...
M. N. Senchev +4 more
doaj +1 more source
Development of Combustion Test Facility for Liquid Rocket Engine [PDF]
, 2006 Dong-Hwan Kim +2 more
openalex +1 more source
The Formation and Properties of Liquid Sheets Suitable for Use in Rocket Engine Injectors [PDF]
Formation and properties of liquid sheets suitable for use in rocket engine ...
Riebling, R. W.
core +1 more source