Results 111 to 120 of about 38,780 (255)

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, Wong, George S., Ziese, James M.   +2 more
core   +1 more source

Effects of Wire-Wrapping Patterns and Low Temperature on Combustion of Propellant Embedded with Metal Wire

Aerospace
Incorporating silver wires into propellant has emerged as a highly effective strategy for enhancing propellant burning rates, a technique extensively deployed in the construction of numerous fielded sounding rockets and tactical missiles.
Qiu Wu, Jiangong Zhao, Quanbin Ren
doaj   +1 more source

NUCLEAR ROCKET PROPULSION. A Selected Bibliography of the Unclassified Literature

, 1961
R.W. comp. Bussard
openalex   +2 more sources

On a choice of optimum operational modes of electrical rocket propulsion system [PDF]

, 2003
В.И. Стаценко, Александр Николаевич Петренко, I. N. Statsenko   +2 more
openalex   +1 more source

Student Activities, Research and Development in High-power Rocket Propulsion and Systems Engineering [PDF]

, 2020
James M. Cook, Maxim Strehle, Jonathan Schaefer, T. Ambro, William Hiser, Andrew Riddle, Sanjay Jayaram   +6 more
openalex   +1 more source

Concepts for the design of an antimatter annihilation rocket [PDF]

Matter-antimatter annihilation is considered for spacecraft propulsion. Annihilation produces considerably more energy per unit mass of propellant than any other known means of energy production. An antimatter annihilation rocket requires several systems
Morgan, D. L., Jr.
core   +1 more source

Numerical Analysis of Solid Rocket Motor Instabilities With AP Composite Propellants [PDF]

, 1999
A non-steady model for the combustion of ammonium perchlorate composite propellants has been developed in order to be incorporated into a comprehensive gasdynamics model of solid rocket motor flow fields.
Beddini, Robert A., Cohen, Norman S., Culick, Fred E. C., Roh, Tae-Seong   +3 more
core  

Analysis of the characteristics of the ejector mode of the pulse detonation propulsion system of the combined acceleration cycle

Авіаційно-космічна техніка та технологія
The subjects of this article are processes in the chamber of the pulse detonation propulsion system of the combined acceleration cycle (PSCA). The goal is to identify the most significant factors and study their influence on the defining characteristics ...
Olena Zolotko, Oleksandr Zolotko, Oleksandr Aksonov, Vitalii Stoliarchuk, Oleksandr Cherniavskyi   +4 more
doaj   +1 more source

THE NUCLEAR ROCKET: NEW POWERPLANT FOR SPACE VEHICLE PROPULSION

, 1960
H.R. Schmidt, R.S. Decker
openalex   +2 more sources

Comparison of the Effects of Using Tygon Tubing in Rocket Propulsion Ground Test Pressure Transducer Measurements [PDF]

, 2005
Rebecca Farr, John Wiley, Patrick J. Vitarius   +2 more
openalex   +1 more source