Results 131 to 140 of about 1,081 (242)

Composition, characterization and performance studies of hybrid rocket motor doped with metallic additives and high entropy alloy

open access: yes
The poor combustion efficiency and low regression rate of the Hybrid Rocket Motor (HRM) limit its use in propulsion systems. Therefore, a thorough examination of the use of high-energy additives such as metals and alloys were carried out to improve the ...
Abd Razak, Najihah   +4 more
core   +1 more source

Development of a Two Dimensional, Optically Accessible, Hybrid Rocket Motor

open access: yes, 2019
Traditionally, launch vehicles and in-space vehicles use solid rocket motors (SRM) and liquid rocket engines (LRE) to propel them into and through space. However, there are many drawbacks to both propulsion systems.
Boyle, Sadie
core  

Investigation of Non-Conventional Bio-Derived Fuels for Hybrid Rocket Motors

open access: yes, 2007
Non-conventional bio-derived fuels have been evaluated for use in hybrid rocket motors. Tests were conducted at combustion pressures in the range of 100 – 220 psig and thrust levels of 40 – 170 newtons.
Putnam, Scott Grayson
core  

Multimatrix Composite Materials for Rocket Nozzle Manufacturing: A Comparative Review. [PDF]

open access: yesPolymers (Basel)
Meiirbekov M   +7 more
europepmc   +1 more source

Simulation Model for Hardware-in-the-Loop Tests of the ILR-33 AMBER Rocket Control System. [PDF]

open access: yesSensors (Basel)
Cieśliński D   +4 more
europepmc   +1 more source

CFD Analysis of the 24-inch JIRAD Hybrid Rocket Motor

open access: yes, 1996
A series of multispecies, multiphase computational fluid dynamics (CFD) analyses of the 24-inch diameter joint government industry industrial research and development (JIRAD) hybrid rocket motor is described.
Ungewitter, Ronald   +2 more
core  

Thermal Insulation Based on NBR-Elastomerized Phenolic Resin Reinforced with Carbon Fibers: Mechanical and Ablation Properties. [PDF]

open access: yesMaterials (Basel)
Gržetić J   +6 more
europepmc   +1 more source

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