Advanced research and technology programs for advanced high-pressure oxygen-hydrogen rocket propulsion [PDF]
A research and technology program for advanced high pressure, oxygen-hydrogen rocket propulsion technology is presently being pursued by the National Aeronautics and Space Administration (NASA) to establish the basic discipline technologies, develop the ...
Marsik, S. J., Morea, S. F.
core +1 more source
Trajectory-correction propulsion system Patent [PDF]
, 1966 Spacecraft trajectory correction propulsion ...
Schmitz, B. W., Smith, W. W.
core +1 more source
Effect of Varying Design Options on the Transient Behavior of a Hybrid Rocket Motor
Journal of Aerospace Technology and Management, 2014 Hybrid rockets provide compelling features for use in atmospheric and space rocket propulsion. One of the prominent applications of hybrid rockets which foster on its characteristics is the propulsion of micro air launch vehicles. In this paper, a set of
Raed Kafafy +2 more
doaj
Modified double base propellants containing RDX with zero burning rate temperature coefficient
Energetic Materials FrontiersLow temperature sensitivity coefficients are of great significance for improving the combustion stability of modified double-base propellants (MDBPs) under sensitive environmental conditions.
Chao Zhang +4 more
doaj +1 more source
Blistering barnacles: Space physiology in The Adventures of Tintin
Experimental Physiology, EarlyView.
Jacob P. Hartmann +4 more
wiley +1 more source
Rocket science unveiled: A differential equation exploration of motion
AlifmatikaThrough the perspective of differential equations, the report "Rocket Science Unveiled" explores the amazing invention of rocket propulsion. In order to study, comprehend, and forecast the behavior of rocket engines, differential equations are essential.
Pravesh Sharma +3 more
doaj +1 more source
National Institute for Rocket Propulsion Systems 2012 Annual Report: A Year of Progress and Challenge [PDF]
The National Institute for Rocket Propulsion Systems (NIRPS) maintains and advances U.S. leadership in all aspects of rocket propulsion for defense, civil, and commercial uses. The Institute's creation is in response to widely acknowledged concerns about
Doreswamy, Rajiv +2 more
core +1 more source
Numerical Analysis of Solid Rocket Motor Instabilities With AP Composite Propellants [PDF]
, 1999 A non-steady model for the combustion of ammonium perchlorate composite propellants has been developed in order to be incorporated into a comprehensive gasdynamics model of solid rocket motor flow fields.
Beddini, Robert A. +3 more
core
Beyond the horizon: Why space biology is the next great innovation opportunity
Experimental Physiology, EarlyView.
Carina Kern, Keith Siew
wiley +1 more source
Combustion of Date Stone and Jojoba Solid Waste in a Hybrid Rocket-like Combustion Chamber
AerospaceThe performance of two solid biomass wastes, date stone and jojoba solid waste, was experimentally examined for their potential application in combustion and propulsion systems.
Saleh B. Alsaidi +2 more
doaj +1 more source