Results 131 to 140 of about 38,437 (282)

Designing and Testing of HDPE–N₂O Hybrid Rocket Engine

Engineering Proceedings
Hybrid Rocket Engines (HREs) combine the advantages of solid and liquid propellants, offering thrust control, simplicity, safety, and cost efficiency.
Triyan Pal Arora, Noah Buttrey, Peter Kirman, Sanmukh Khadtare, Eeshaan Kamath, Dario del Gatto, Adriano Isoldi   +6 more
doaj   +1 more source

Design Optimization of Gas Generator Hybrid Propulsion Boosters [PDF]

A methodology used in support of a study for NASA/MSFC to optimize the design of gas generator hybrid propulsion booster for uprating the National Space Transportation System (NSTS) is presented.
Fink, Larry, Phillips, Dwight, Weldon, Vincent   +2 more
core   +2 more sources

A Preliminary Study of the Wet Towel Hybrid Rocket Motor.

, 1997
Harunori Nagata, R. Akiba, Nobuhiro Tanatsugu, Masahiro Kohno, Rikio Yokota, Seiyu Kayuta   +5 more
openalex   +2 more sources

Physical foundation for the construction of paraffin-based hybrid rocket engines. Кinetics of melting and combustion [PDF]

, 2011
Olena Aktan, Yu. F. Zabashta, Valeriy Chernyak, S. G. Orlovskaya, O.S. Svechnikova, F.F. Karimova, М. С. Шкоропадо   +6 more
openalex   +1 more source

From Earth to Orbit: An assessment of transportation options [PDF]

The report assesses the requirements, benefits, technological feasibility, and roles of Earth-to-Orbit transportation systems and options that could be developed in support of future national space programs.
Blond, Edmund, Brill, Yvonne C., Budiansky, Bernard, Cooper, Robert S., Demisch, Wolfgang H., Gavin, Joseph G., Jr., Hawk, Clark W., Kerrebrock, Jack L., Lichtenberg, Byron K., Mager, Artur   +9 more
core   +1 more source

A Preliminary Study of End-Burning Hybrid Rocket. Part 2. Combustion Characteristics.

, 2001
Nozomu Hashimoto, Takahiro Katō, Harunori Nagata, Isao Kudo   +3 more
openalex   +1 more source

A Unique Hybrid Propulsion System Design for Large Space Boosters [PDF]

A study was made of the application of hybrid rocket propulsion technology to large space boosters. Safety, reliability, cost, and performance comprised the evaluation criteria, in order of relative importance, for this study.
Rodgers, Frederick C.
core   +1 more source

712 A Reusable Hybrid Rocket System : Its Nominal Design and Flight Capability Predictions

, 2001
Hiroshi Yoshida, Jun Nakaya, Naoki Maeda, Kazuhide MIZOBATA, Hiromu Sugiyama, Harunori Nagata, Ken'ichi ITOH, Ryojiro Akiba, Yoichi OOWADA   +8 more
openalex   +2 more sources

Approaches to Low Fuel Regression Rate in Hybrid Rocket Engines [PDF]

, 2012
Dario Pastrone
openalex   +1 more source

Near-future rocket launches could slow ozone recovery. [PDF]

NPJ Clim Atmos Sci
Revell LE, Bannister MT, Brown TFM, Sukhodolov T, Vattioni S, Dykema J, Frame DJ, Cater J, Chiodo G, Rozanov E.   +9 more
europepmc   +2 more sources