Lightweight RepVGG-Based Cross-Modality Data Prediction Method for Solid Rocket Motors. [PDF]
Yang H, Zheng S, Wang X, Xu M, Li X.
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
core +1 more source
Near-future rocket launches could slow ozone recovery. [PDF]
Revell 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.
core +1 more source
Nano-Iron as a Catalyst in Isocyanate-Free Rocket Propellants. [PDF]
Chmielarek M +2 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
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
Space Transportation System solid rocket booster thrust vector control system [PDF]
The Solid Rocket Booster, Thrust Vector Control (TVC) system was designed in accordance with the following requirements: self-contained power supply, failsafe operation, 20 flight uses after exposure to seawater landings, optimized cost, and component ...
Mccool, A. A. +2 more
core +1 more source
Experimental Study on the Evolution of Mechanical Properties and Their Mechanisms in a HTPB Propellant Under Fatigue Loading. [PDF]
Feng F +5 more
europepmc +1 more source
Coupled simulations of solid rocket motors [PDF]
I. Parsons +5 more
openaire +1 more source

