Results 121 to 130 of about 29,759 (245)

Engineering and programming manual: Two-dimensional kinetic reference computer program (TDK) [PDF]

open access: yes
The Two Dimensional Kinetics (TDK) computer program is a primary tool in applying the JANNAF liquid rocket thrust chamber performance prediction methodology.
Coats, D. E.   +2 more
core   +1 more source

Liquid rocket engine axial-flow turbopumps [PDF]

open access: yes
The axial pump is considered in terms of the total turbopump assembly. Stage hydrodynamic design, pump rotor assembly, pump materials for liquid hydrogen applications, and safety factors as utilized in state of the art pumps are among the topics ...
Farquhar, J.   +4 more
core   +1 more source

Reliability evaluation methodology for NASA applications [PDF]

open access: yes
Liquid rocket engine technology has been characterized by the development of complex systems containing large number of subsystems, components, and parts. The trend to even larger and more complex system is continuing.
Taneja, Vidya S.
core   +1 more source

Method for Determining Optimum Injector Inlet Geometry [PDF]

open access: yes
A method for determining the optimum inlet geometry of a liquid rocket engine swirl injector includes obtaining a throttleable level phase value, volume flow rate, chamber pressure, liquid propellant density, inlet injector pressure, desired target spray
Myers, W. Neill, Trinh, Huu P.
core   +1 more source

The alleged contributions of Pedro E. Paulet to liquid-propellant rocketry [PDF]

open access: yes
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
core   +1 more source

Cryogenic combustion laboratory [PDF]

open access: yes
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

Large Liquid Rocket Testing: Strategies and Challenges [PDF]

open access: yes
Rocket propulsion development is enabled by rigorous ground testing in order to mitigate the propulsion systems risks that are inherent in space flight.
Hebert, Bartt J., Rahman, Shamim A.
core   +1 more source

Multimatrix Composite Materials for Rocket Nozzle Manufacturing: A Comparative Review. [PDF]

open access: yesPolymers (Basel)
Meiirbekov M   +7 more
europepmc   +1 more source

JANNAF "Test and Evaluation Guidelines for Liquid Rocket Engines": Status and Application [PDF]

open access: yes
For many decades, the U.S. rocket propulsion industrial base has performed remarkably in developing complex liquid rocket engines that can propel critical payloads into service for the nation, as well as transport people and hardware for missions that ...
Parkinson, Douglas   +2 more
core   +1 more source

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