A logistics and potential hazard study of propellant systems for a Saturn 5 derived heavy lift (three-stage core) launch vehicle [PDF]
The Bush Administration has directed NASA to prepare for a return to the Moon and on to Mars - the Space Exploration Initiative. To meet this directive, powerful rocket boosters will be required in order to lift payloads that may reach the half-million ...
Whitney, E. Dow
core +1 more source
A versatile low-cost data acquisition system for small rocket engine test bench. [PDF]
Netzel NA +3 more
europepmc +1 more source
Pulse performance analysis for small hypergolic-propellant rocket engines [PDF]
Small rocket engine tests were conducted for the purpose of obtaining pulse performance data to aid in preliminary design and evaluation of attitude control systems.
Sforzini, R. H., Smith, G. W.
core +1 more source
Multimatrix Composite Materials for Rocket Nozzle Manufacturing: A Comparative Review. [PDF]
Meiirbekov M +7 more
europepmc +1 more source
Study of Thixotropic Characteristics of a Kerosene Gel Propellant by Bayesian Optimization. [PDF]
Zhou H +5 more
europepmc +1 more source
Operationally Efficient Propulsion System Study (OEPSS) data book. Volume 4: OEPSS design concepts [PDF]
This study was initiated to identify operations problems and cost drivers for current propulsion systems and to identify technology and design approaches to increase the operational efficiency and reduce operations costs for future propulsion systems. To
Farhangi, Shahram +2 more
core +1 more source
Liquid Carbon-Boron Cluster Additives for Mixed Amine-50. [PDF]
Mu X, Wang S, Yang F, Li H.
europepmc +1 more source
Experimental Study on the Unsteady Spray Combustion Process of a Liquid Oxygen/Methane Swirl Coaxial Injector. [PDF]
Cao P, Bai X, Li Q, Cheng P, Li Z.
europepmc +1 more source
Orbital biomanufacturing: the key to space resiliency, operational persistence, and ethical sustainability. [PDF]
Younger AK.
europepmc +1 more source
Effects of NO in oxidant and initial temperature on working characteristics of MON-X/MMH liquid space thruster. [PDF]
Zhou YH +5 more
europepmc +1 more source

