Results 141 to 150 of about 38,437 (282)

3D printed hybrid rocket fuels with μAl core-shell particles coated with polyvinylidene fluoride and polydopamine: Enhanced combustion characteristics

Defence Technology
3D printing technology enhances the combustion characteristics of hybrid rocket fuels by enabling complex geometries. However, improvements in regression rates and energy properties of monotonous 3D printed fuels have been limited.
Qihang Chen, Xiaolong Fu, Weitao Yang, Suhang Chen, Zhiming Guo, Rui Hu, Huijie Zhang, Lianpeng Cui, Xu Xia   +8 more
doaj  

713 Development of Aerial Vehicle for Fly-back Hybrid-Rocket : The Avionics of the Winged Vehicle control

, 2001
Tuyoshi Takada, Kuniaki TOYODA, Seiichi Ohtaki, Ryuichi Mitsuhashi, Sin SATORI, Harunori Nagata, Yoshinori Aoki   +6 more
openalex   +2 more sources

Mass Flow Rate and Isolation Characteristics of Injectors for Use with Self-Pressurizing Oxidizers in Hybrid Rockets [PDF]

, 2013
Benjamin S. Waxman, Brian Cantwell, Greg Zilliac, Jonah E. Zimmerman   +3 more
openalex   +1 more source

Effect of tangential swirl air inlet angle on the combustion efficiency of a hybrid powder-solid ramjet [PDF]

, 2019
ANSYS Inc, Ao, Betelin, Cai, Chang, Chelaru, Chen, dawara, Gany, Gany, Glassman, Goroshin, Haijun Sun, Hu, Humberto Medina, Hussmann, Hussmann, Jung, Kalpakli, Kazaoka, King, Li, Li, Liang, Loftus, Magnussen, Meinköhn, Morsi, Musa, Musa, NASA, Natan, Nie, Pern, Pern, Povitsky, Rashkovskiy, Rodić, Rui Jia, Sandall, Sender, Shih, Shorr, Varghese, Wang, Xia, Xia, Xu, Yeh, Yihua Xu   +49 more
core   +1 more source

Magnetoplasma sheath waves on a conducting tether in the ionosphere with applications to EMI propagation on large space structures [PDF]

A recent space experiment confirmed sheath-wave propagation of a kilometer-long insulated wire in the ionosphere, oriented parallel to the Earth's magnetic field.
Balmain, K. G., Bantin, C. C., James, H. G.   +2 more
core   +1 more source

A Study on the Combustion Instability of the Hybrid Rocket Motor with a Diaphragm [PDF]

, 2013
Jungpyo Lee, Youngnam Kim, Jinkon Kim, Heejang Moon   +3 more
openalex   +1 more source

Design Optimization and Parameter Analysis of a Hybrid Rocket Motor-Powered Small LEO Launch Vehicle [PDF]

, 2021
Hao Zhu, Pengcheng Wang, Weile Xu, Yuanjun Zhang, Hui Tian, Guobiao Cai   +5 more
openalex   +1 more source

Development of a Winged Vehicle for Fly-back Hybrid-rocket : Development of the Launch Equipment for a Winged Vehicle

, 2002
Kuniaki SHIBA, Ayako SHIMOOKA, Akihiro MATSUO, Akira Nabae, Kuniaki TOYODA, Shin Satori, Ryuichi Mitsuhashi, Harunori Nagata   +7 more
openalex   +2 more sources

Correction to: A Computational Tool for the Design of Hybrid Rockets [PDF]

, 2021
Paolo Maria Zolla, Mario Tindaro Migliorino, Daniele Bianchi, Francesco Nasuti, Rocco Carmine Pellegrini, Enrico Cavallini   +5 more
openalex   +1 more source

Plasma structuring within an expanded polar cap and cusp studied with the SS-520-3 sounding rocket. [PDF]

Earth Planets Space
Buschmann LM, Asamura K, Clausen LBN, Jin Y, Kojima H, Kumamoto A, Kurita S, Ogawa Y, Oksavik K, Saito Y, Spicher A, Yokota S, Miloch WJ.   +12 more
europepmc   +2 more sources