Results 71 to 80 of about 826 (185)

Optimization design of anti-creep reinforcement structure for solid rocket motor propellant grain

Jixie qiangdu
To address the creep issue that arises during the long-term vertical storage of solid rocket motor (SRM), a method was proposed that involved embedding a specially shaped functional combustible core model (reinforcement structure)into the propellant ...
LIU Mengyang, GAO Jingwei, YAN Bo, ZHANG Xiaofei   +3 more
doaj  

Analysis of carbon nano particle variant as the propellant fuel to increase specific impulses of rockets [version 3; peer review: 1 approved, 2 approved with reservations]

F1000Research
Background This study compares propellant fuels’ specific thrust and impulse parameters using nanocarbon variant fuels from coconut shells and coal. Specific impulses and impulses are essential parameters that determine rocket performance.
MAE Hafizah, Y Ruyat, RDA Navalino, NRS Muda   +3 more
doaj   +1 more source

Development and testing of the solid fuel power plant axisymmetric model applied to regimes of combustion chamber dynamic instability

Авіаційно-космічна техніка та технологія
Innovative use of energy resources in deep space planets is a technology that allows a significant increase in space exploration based on the design of rocket power plants, particularly for lunar landing modules using (Lunar Regolith) propellants ...
Olexiy Nikolayev, Inna Bashliy
doaj   +1 more source

Solid propellant rocket motors [PDF]

, 2006
openaire   +2 more sources

Impact of Selected Metal Oxides on the Thermodynamics of Solid Rocket Propellant Combustion. [PDF]

Molecules
Janowska K, Waśkiewicz S, Skóra P, Hawelek L, Prasuła P, Jarosz T, Stolarczyk A.   +6 more
europepmc   +1 more source

Flexible Three-Dimensional Stress Sensor for Embedded Monitoring of Solid Rocket Propellant. [PDF]

Micromachines (Basel)
Shi Y, Lü X, Ren K, Zhu W.
europepmc   +1 more source

First applications of ultrasound technology in solid rocket propellant combustion promotion. [PDF]

Ultrason Sonochem
Wen Z, Jing H, Hao F, Wang Y, Kuang B, Liu P, Ao W.   +6 more
europepmc   +1 more source

Mesoscopic Damage Characteristics of NEPE Propellant Under Drop-Weight Impact. [PDF]

Materials (Basel)
Zhang Z, Sun Z, Liu Y, Zhu Y, Hu Y.
europepmc   +1 more source

Study on Creep Mechanical Properties of HTPB Solid Propellant. [PDF]

Materials (Basel)
Jin L, Jia S, Zhang Z, An Z, Lu Z.
europepmc   +1 more source

Meso-Scale Observations of the Evolution of Matrix/Filler Interface Dewetting During NEPE Propellant Aging. [PDF]

Polymers (Basel)
Chen Z, Wang X, Zou Z, Qiang H, Wang M, Wu Y.   +5 more
europepmc   +1 more source