Results 71 to 80 of about 11,032 (271)
Current activities at IITRI on high- temperature protective coatings [PDF]
Heat resistant protective coatings for use in liquid propellant rocket ...
Hess, A. L.+2 more
core +1 more source
Tank construction for space vehicles Patent [PDF]
Liquid propellant tank design with semitoroidal ...
Blumrich, J. F., Loy, C. A.
core +1 more source
Fluid Dynamics and Infrared Stealth of Marine IRS Devices: A Review
ABSTRACT Infrared suppression (IRS) devices for naval ships play a crucial role in reducing the infrared radiation signature of high‐temperature exhaust, thereby enhancing the survivability of ships against infrared‐guided weapons. This paper provides a comprehensive review of recent advancements in the design and optimization of IRS devices.
Yitao Zou+5 more
wiley +1 more source
Simple Learning-Based Robust Nonlinear Control of an Electric Pump for Liquid-Propellant Rocket Engines [PDF]
Mohammad Jafari+2 more
openalex +1 more source
Liquid rocket performance computer model with distributed energy release Interim final report, 15 Aug. 1969 - 15 Aug. 1970 [PDF]
Liquid propellant rocket engine performance computer program with distributed energy ...
Campell, D. T.+2 more
core +1 more source
Rocket engine injector Patent [PDF]
Rocket engine injector orifice to accommodate changes in density, velocity, and pressure, thereby maintaining constant mass flow rate of propellant into rocket combustion ...
Stein, S.
core +1 more source
ABSTRACT Nitramine propellants have attracted considerable attention in the domain of solid rockets and gun propulsion because of their energetic and smokeless features. Ammonium perchlorate (AP) is the widely used oxidizer in propellants owing to the excellent burning characteristics.
Makoto Kohga+2 more
wiley +1 more source
The prediction of the nonlinear behavior of unstable liquid rockets [PDF]
Analytical technique for solving nonlinear combustion problems associated with liquid propellant rocket ...
Powell, E. A., Zinn, B. T.
core +1 more source
Design criteria monograph on turbopump systems [PDF]
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
Small rocket engine Patent [PDF]
Regenerative cooling system for small rocket engine having restart capability and using noncryogenic hypergolic ...
Latto, W. T., Jr.
core +1 more source