Results 111 to 120 of about 940 (232)
Hydrodynamic Instabilities Modeling in Hybrid Rocket Engines
第1回ハイブリッドロケットシンポジウム(2018年6月28日-29日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県 1st Hybrid Rocket Symposium (June 28-29, 2018. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan 資料番号: SA6000126012 レポート番号: HR-2018 ...
openaire
Advances in Structural Reliability Analysis of Solid Propellant Grain: A Comprehensive Review. [PDF]
Tang C +4 more
europepmc +1 more source
Modeling fatigue damage evolution in CMDB propellant based on dynamic modulus. [PDF]
Yao L +4 more
europepmc +1 more source
Hybrid rocket engine on the methane clathrate
A.S. Levenko +3 more
openaire +1 more source
Influence of plasma-enhanced combustion on RBCC engine using URANS. [PDF]
Zhang WR, Liu YS, Zou XR, Xu C, Xue R.
europepmc +1 more source
Simulation Model for Hardware-in-the-Loop Tests of the ILR-33 AMBER Rocket Control System. [PDF]
Cieśliński D +4 more
europepmc +1 more source
Multiphysics Analysis of Hydroxyl-terminated Polybutadiene Regression in Hybrid Rocket Engines
MIGLIORINO Mario Tindaro +4 more
openalex +1 more source

