Results 161 to 170 of about 38,278 (273)
Effect of gaseous and solid simulated jet plumes on an 040A space shuttle launch configuration at m=1.6 to 2.2 [PDF]
The effect of plume-induced flow separation and aspiration effects due to operation of both orbiter and the solid rocket motors on a 0.019-scale model of the launch configuration of the Space Shuttle Vehicle is determined.
Blackwell, K. L. +5 more
core +1 more source
Available analyses and material property information are summarized relevant to the design of four rocket motor nozzles currently incorporated in the four solid propellant rocket stages of the NASA SCOUT launch vehicle.
Shieds, S.
core +1 more source
Near-future rocket launches could slow ozone recovery. [PDF]
NPJ Clim Atmos SciRevell LE +9 more
europepmc +2 more sources
Ignition overpressure study from solid rocket motor firings [PDF]
The objective was to investigate, through experimental means, the basic mechanisms influencing ignition overpressure and to determine ways to suppress ignition overpressure. Ignition overpressure was studied using solid rocket motors with geometry scaled
Counter, Douglas D.
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Impact of Selected Metal Oxides on the Thermodynamics of Solid Rocket Propellant Combustion. [PDF]
MoleculesJanowska K +6 more
europepmc +1 more source
Ice nuclei measurements from solid rocket motor effluents [PDF]
The ice crystal forming nuclei (IN) measured in solid rocket motor (SRM) exhaust products is discussed in relation to space shuttle exhaust. Preliminary results from laboratory investigations and flight preparations for March 1978 Titan launch are ...
Hindman, E. E., II
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Nano-Iron as a Catalyst in Isocyanate-Free Rocket Propellants. [PDF]
Polymers (Basel)Chmielarek M +2 more
europepmc +1 more source
Demonstration of a sterilizable solid rocket motor system [PDF]
A solid propellant rocket motor containing 60.9 Kg (134-lb) of propellant was successfully static fired after being subjected to eight heat sterilization cycles (three 54-hour cycles plus five 40-hour cycles) at 125 C (257 F).
Lambert, W. L. +2 more
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Numerical Simulation of Failure Modes of Solid Propellants with Internal Cavities Under Various Loading Conditions. [PDF]
Polymers (Basel)Liu K, Yang Q, Cao L, Wang J, Cao P.
europepmc +1 more source
Studies of the exhaust products from solid propellant rocket motors [PDF]
This study was undertaken to determine the feasibility of conducting environmental chamber tests on the physical processes which occur when a solid rocket motor exhaust mixes with the ambient atmosphere. Of particular interest was the interaction between
Dawbarn, R., Kinslow, M.
core +1 more source