Influence of plasma-enhanced combustion on RBCC engine using URANS. [PDF]
Sci RepZhang WR, Liu YS, Zou XR, Xu C, Xue R.
europepmc +1 more source
Design Office of Liquid Rocket Engines is 60 [PDF]
Kosmičeskaâ tehnika. Raketnoe vooruženie, 2018 V. A. Shulga, A. V. Dibrivny
openaire +1 more source
Large Liquid Rocket Testing: Strategies and Challenges [PDF]
Rocket propulsion development is enabled by rigorous ground testing in order to mitigate the propulsion systems risks that are inherent in space flight.
Hebert, Bartt J., Rahman, Shamim A.
core +1 more source
Design and Manufacturing of Experimental Solid Propellant Rocket Motor Cases Made of Carbon Composite Materials. [PDF]
Polymers (Basel)Baiserikov B +7 more
europepmc +1 more source
Spray combustion under oscillatory pressure conditions [PDF]
The performance and stability of liquid rocket engines is often argued to be significantly impacted by atomization and droplet vaporization processes.
Jacobs, H. R., Santoro, R. J.
core +1 more source
Proposals for Improving the Efficiency and Durability of the Turbines of Turbo-Pump Assemblies in Liquid-Propellant Rocket Engines by Using Double-Sided Crest-Type Radial Labyrinth Seals [PDF]
, 2019 V S Vasiliev +3 more
openalex +1 more source
Liquid Carbon-Boron Cluster Additives for Mixed Amine-50. [PDF]
MoleculesMu X, Wang S, Yang F, Li H.
europepmc +1 more source
Liquid Rocket Booster (LRB) for the Space Transportation System (STS) systems study. Appendix C: Battery report for the liquid rocket booster TVC actuators [PDF]
The actuators for control of engine valves and gimbals for a booster require 165 kW or more peak power at 270 volts direct current (VDC) during the 2 or 3 minutes of first stage ascent; other booster devices require much less power at 28 VDC.
core +1 more source
Effects of NO in oxidant and initial temperature on working characteristics of MON-X/MMH liquid space thruster. [PDF]
Sci ProgZhou YH +5 more
europepmc +1 more source