Small hydrogen/oxygen rocket flowfield behavior from heat flux measurements [PDF]
The mixing and heat transfer phenomena in small rocket flow fields with fuel film cooling is not well understood. An instrumented, water-cooled chamber with a gaseous hydrogen/gaseous oxygen injector was used to gather steady-state inner and outer wall ...
Reed, Brian D.
core +1 more source
Solid rocket technology advancements for space tug and IUS applications [PDF]
In order for the shuttle tug or interim upper stage (IUS) to capture all the missions in the current mission model for the tug and the IUS, an auxiliary or kick stage, using a solid propellant rocket motor, is required.
Ascher, W. +3 more
core +1 more source
Propulsion technology needs for advanced space transportation systems [PDF]
Plans are formulated for chemical propulsion technology programs to meet the needs of advanced space transportation systems from 1980 to the year 2000.
Gregory, J. W.
core +1 more source
SSME propulsion performance reconstruction techniques [PDF]
In view of the complex flight operation of the Space Shuttle propulsion system together with an expected launch rate increase, the flight performance reconstruction process needs to be performed by automated computer programs.
Temple, Enoch C.
core +1 more source
A dynamic simulation approach to optimize thrust regulation in electric pump-fed rocket engines. [PDF]
Li T, He H, Yu N, Sun X, Cai G.
europepmc +1 more source
Cryogenic combustion laboratory [PDF]
The objective is to establish a major experimental laboratory for studying fundamental processes such as mixing and combustion under liquid rocket engine conditions.
Kuo, Kenneth K., Santoro, R. J.
core +1 more source
Advanced Nanomaterials and Energetic Application: Experiment and Simulation. [PDF]
Pang W, Trache D, Zhang K.
europepmc +1 more source
Next generation earth-to-orbit space transportation systems: Unmanned vehicles and liquid/hybrid boosters [PDF]
The United States civil space effort when viewed from a launch vehicle perspective tends to categorize into pre-Shuttle and Shuttle eras. The pre-Shuttle era consisted of expendable launch vehicles where a broad set of capabilities were matured in a ...
Hueter, Uwe
core +1 more source
Application of Gaussian SVM Flame Detection Model Based on Color and Gradient Features in Engine Test Plume Images. [PDF]
Yan S, Gao Y, Zhang Z, Li Y.
europepmc +1 more source
Multimatrix Composite Materials for Rocket Nozzle Manufacturing: A Comparative Review. [PDF]
Meiirbekov M +7 more
europepmc +1 more source

