Near-future rocket launches could slow ozone recovery. [PDF]
NPJ Clim Atmos SciRevell LE +9 more
europepmc +2 more sources
Impact of Selected Metal Oxides on the Thermodynamics of Solid Rocket Propellant Combustion. [PDF]
MoleculesJanowska K +6 more
europepmc +1 more source
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]
Polymers (Basel)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
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
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
A dynamic simulation approach to optimize thrust regulation in electric pump-fed rocket engines. [PDF]
Sci RepLi T, He H, Yu N, Sun X, Cai G.
europepmc +1 more source
NASA Lewis Thermal Barrier Feasibility Investigated for Use in Space Shuttle Solid-Rocket Motor Nozzle-to-Case Joints [PDF]
Assembly joints of modern solid-rocket motor cases are usually sealed with conventional O-ring seals. The 5500 F combustion gases produced by rocket motors are kept a safe distance away from the seals by thick layers of insulation and by special ...
Dunlap, Patrick H., Jr. +1 more
core +1 more source
Experimental Study on the Evolution of Mechanical Properties and Their Mechanisms in a HTPB Propellant Under Fatigue Loading. [PDF]
Polymers (Basel)Feng F +5 more
europepmc +1 more source