Results 171 to 180 of about 863,762 (375)
Handbook of Recommended Practices for the Determination of Liquid Monopropellant Rocket Engine Performance, [PDF]
R. A. Bjorklund+2 more
openalex +1 more source
➢ A one‐step selective laser reaction pyrolysis (SLRP) technique was developed to rapidly synthesize hafnium carbide (HfC) from liquid polymer precursors. ➢ XRD and TEM confirmed the nanocrystalline structure of the HfC. ➢ The SLRP‐based process achieved up to 54% ceramic yield, 18% higher than furnace‐based methods.
Shalini Rajpoot+3 more
wiley +1 more source
Fiber-reinforced ceramic composites for Earth-to-orbit rocket engine turbines [PDF]
Fiber reinforced ceramic matrix composites (FRCMC) are emerging materials systems that offer potential for use in liquid rocket engines. Advantages of these materials in rocket engine turbomachinery include performance gain due to higher turbine inlet ...
Brockmeyer, Jerry W.+1 more
core +1 more source
Alloparenting the investment child: A reply to responses
The British Journal of Sociology, EarlyView.
Nina Bandelj
wiley +1 more source
From Bednets to Rocket Ships: Efficiency in the Long‐Term and Neglect for the Present
ABSTRACT In this article I develop an objection to Longtermism – the view that concern for the long‐term future is a moral imperative – that is often gestured at, but not fleshed out. I call this the Far‐Future Priority Objection: Longtermism may entail significant resource reallocation and systemic neglect of the worst off today.
Elizabeth C. Hupfer
wiley +1 more source
Experimental validation of rotating detonation for rocket propulsion. [PDF]
Bennewitz JW+14 more
europepmc +1 more source
The development of a post-test diagnostic system for rocket engines [PDF]
An effort was undertaken by NASA to develop an automated post-test, post-flight diagnostic system for rocket engines. The automated system is designed to be generic and to automate the rocket engine data review process.
Zakrajsek, June F.
core +1 more source
Fluid thrust control system [PDF]
A pure fluid thrust control system is described for a pump-fed, regeneratively cooled liquid propellant rocket engine. A proportional fluid amplifier and a bistable fluid amplifier control overshoot in the starting of the engine and take it to a ...
Howell, W. L.+2 more
core +1 more source