Results 121 to 130 of about 1,081 (242)

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HemaSphere, Volume 10, Issue S1, June 2026.
wiley   +1 more source

Development and Performance of the 10 kN Hybrid Rocket Motor for the Stratos II Sounding Rocket

, 2016
This paper presents the development work of the 10 kN hybrid rocket motor DHX-200 Aurora. The DHX-200 Aurora was developed by Delft Aerospace Rocket Engineering (DARE) to power the Stratos II and Stratos II+ sounding rocket, with the later one being ...
Wink, J (author), Ehlen, J, Cervone, A., Ehlen, J (author), Zandbergen, B.T.C. (author), Knop, T.R., Wieling, W (author), Wink, J, Huijsman, R, Zandbergen, B.T.C., Werner, R.M. (author), Wieling, W, Powell, S (author), Florea, R., Powell, S, Florea, R. (author), Werner, R.M., Knop, T.R. (author), Cervone, A. (author), Huijsman, R (author)   +19 more
core  

Lightweight RepVGG-Based Cross-Modality Data Prediction Method for Solid Rocket Motors. [PDF]

Sensors (Basel), 2023
Yang H, Zheng S, Wang X, Xu M, Li X.
europepmc   +1 more source

Simulation of wheel type fuel grain in hybrid rocket motor

, 2013
till today, with issues specifically related to combustion instability and lowered regression rate. Simulation is used as a tool to investigate the behavior of hybrid rocket grains under varied operating conditions.
Azami, Muhammad Hanafi, Kafafy, Raed, Idres, Moumen   +2 more
core  

Mixing enhancement in hybrid rocket motor using vortex generators

, 2012
A hybrid rocket is a compromise between a solid and a liquid rocket motor: uses a solid fuel and a liquid oxidizer. This configuration has several well known advantages, such as less security problems, smaller costs, etc.
GIANGI, Marilena, STELLA, Fulvio, NARDECCHIA, FABIO, D. Barbagallo   +3 more
core  

Analysis of carbon nano particle variant as the propellant fuel to increase specific impulses of rockets. [PDF]

F1000Res, 2023
Navalino R, Muda N, Hafizah M, Ruyat Y.
europepmc   +1 more source

DESIGN OF AN AEROSPIKE NOZZLE FOR A HYBRID ROCKET

, 2008
This document describes the design of an axisymmetric aerospike nozzle to replace the conical converging-diverging nozzle of a commercially available hybrid rocket motor.
Gould, Cedric Oldfield, Gould, Cedric O
core  

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

Immersive Virtual Reality for Stroke Rehabilitation: Linking Clinical and Digital Measures of Motor Recovery-A Pilot Study. [PDF]

Bioengineering (Basel)
Ion LA, Săndulescu MI, Potcovaru CG, Poenaru D, Comișel AD, Ștefureac Ș, Lambru AC, Moldoveanu A, Anghel AM, Cinteză D.   +9 more
europepmc   +1 more source

Regression rate determination of a gas generator hybrid rocket motor with GOX

, 2015
Hybrid rocket motors suffer from low regression rates when compared to traditional solid rocket motors. This work investigates the regression rate of a mixed oxidizer hybrid motor using a fuel-rich solid grain with and without gaseous oxygen as an ...
Mascaro, Michael D.
core