Results 161 to 170 of about 14,137 (299)

Analytical study of nozzle performance for nuclear thermal rockets [PDF]

Nuclear propulsion has been identified as one of the key technologies needed for human exploration of the Moon and Mars. The Nuclear Thermal Rocket (NTR) uses a nuclear reactor to heat hydrogen to a high temperature followed by expansion through a ...
Davidian, Kenneth O., Kacynski, Kenneth J.   +1 more
core   +1 more source

Current Implementation Status of Cold Spray Technology: A Short Review. [PDF]

J Therm Spray Technol, 2022
Sun W, Chu X, Lan H, Huang R, Huang J, Xie Y, Huang J, Huang G.   +7 more
europepmc   +1 more source

Comparative Studies of Heat Transfer Coefficients for Rocket Nozzle [PDF]

, 2012
Heecheol Hahm, Yoon‐Goo Kang
openalex   +1 more source

Atomization Characteristics of Hydrogen Peroxide Solutions in Electrostatic Field. [PDF]

Micromachines (Basel), 2022
Huang X, Sheng L, Lu Y, Li S.
europepmc   +1 more source

Transition mechanisms in hypersonic wind-tunnel nozzles: a methodological approach using global linear stability analysis [PDF]

arXiv
Base-flow computations and stability analyses are performed for a hypersonic wind tunnel nozzle at a Mach number of 6. Isothermal and adiabatic wall boundary conditions are investigated, and moderate stagnation conditions are used to provide representative scenarios to study the transition in quiet hypersonic wind tunnel facilities.
arxiv  

The Transfer Functions of Rocket Nozzles [PDF]

, 2012
H.S. Tsien
openalex   +1 more source

Reduced Reaction Mechanism for Rocket Nozzle Ablation Simulations [PDF]

, 2017
Peter Cross, Iain D. Boyd
openalex   +2 more sources

Numerical Investigation of Transonic Flow-Induced Spontaneous Condensation in Micro-Ejector Nozzles. [PDF]

Micromachines (Basel), 2023
Han Y, Wang X, Wang W, Lee YX, Li A.
europepmc   +1 more source

Analysis of SRM model nozzle calibration test data in support of IA12B, IA12C and IA36 space shuttle launch vehicle aerodynamics tests [PDF]

Variations of nozzle performance characteristics of the model nozzles used in the Space Shuttle IA12B, IA12C, IA36 power-on launch vehicle test series are shown by comparison between experimental and analytical data. The experimental data are nozzle wall
Baker, L. R., Jr., Penny, M. M., Tevepaugh, J. A.   +2 more
core   +1 more source

1303 2D-CFD Calculation of Transient Side Thrust at Rocket Nozzle

, 2001
Ryo Morita, Kouichi YONEZAWA, Kazuhiko YOKOTA, Yoshinobu TSUJIMOTO, Norio Sakazume   +4 more
openalex   +2 more sources