Results 71 to 80 of about 940 (232)

Launch support: Managing complementor bottlenecks in the disruptive innovation of small satellites

open access: yesStrategic Management Journal, Volume 47, Issue 3, Page 758-803, March 2026.
Abstract Research Summary Through both qualitative and quantitative analyses of large‐rocket providers' support for small‐satellite manufacturers before the emergence of small rockets, we examine how disruptors to an incumbent ecosystem gain support from complementors of the incumbent technology.
Yue Song, Yue Maggie Zhou, Xiaoping Zhao
wiley   +1 more source

The Role of Creativity and Innovation Management Research in Times of Changing Security and Defence Realities

open access: yesCreativity and Innovation Management, Volume 35, Issue 1, Page 84-90, March 2026.
ABSTRACT Geopolitical uncertainties and the resurgence of security and defence needs present both opportunities and challenges for creativity and innovation management. At both the organizational and the individual levels, we are confronted with multiple ethically challenging choices. Given the changing global security and defence realities, we outline
Mette Præst Knudsen   +4 more
wiley   +1 more source

Hybrid Rocket Engine Burnback Simulations Using Implicit Geometry Descriptions

open access: yesAerospace
The performance of hybrid rocket engines is significantly influenced by the fuel geometry. Burnback simulations, to determine the fuel surface and fluid volume, are therefore an important tool for preliminary design.
Jan Erik Zeriadtke   +2 more
doaj   +1 more source

Investigation of Dual-Vortical-Flow Hybrid Rocket Engine without Flame Holding Mechanism

open access: yesInternational Journal of Aerospace Engineering, 2018
A 250 kgf thrust hybrid rocket engine was designed, tested, and verified in this work. Due to the injection and flow pattern of this engine, this engine was named dual-vortical-flow engine.
A. Lai   +5 more
doaj   +1 more source

Multiphysics Modelling of a Hybrid Rocket Engine [PDF]

open access: yes14th WCCM-ECCOMAS Congress, 2021
Ferrero, A.   +3 more
openaire   +2 more sources

The Application of Computational Thermo-Fluid-Dynamics to the Simulation of Hybrid Rocket Internal Ballistics with Classical or Liquefying Fuels: A Review

open access: yesAerospace, 2019
The computational fluid dynamics of hybrid rocket internal ballistics is becoming a key tool for reducing the engine operation uncertainties and development cost as well as for improving experimental data analysis.
Giuseppe Daniele Di Martino   +3 more
doaj   +1 more source

Study on Thermal Degradation Characteristics and Regression Rate Measurement of Paraffin-Based Fuel

open access: yesEnergies, 2015
Paraffin fuel has been found to have a regression rate that is higher than conventional HTPB (hydroxyl-terminated polybutadiene) fuel and, thus, presents itself as an ideal energy source for a hybrid rocket engine.
Songqi Hu   +4 more
doaj   +1 more source

Analysis of advanced cooling strategies for rocket engines conveying ternary hybrid nanofluids with second slip conditions and melting heat transfer

open access: yesCase Studies in Thermal Engineering
Effective cooling in rocket engines is essential to prevent overheating and ensure efficient performance under extreme operating conditions. This study presents a comprehensive investigation into advanced cooling strategies for rocket engines utilizing ...
Hatem Gasmi   +7 more
doaj   +1 more source

Design Mode Analysis of Pareto Solution Set for Decision-Making Support

open access: yesJournal of Applied Mathematics, 2014
Decision making in engineering design problems is challenging because they have multiple and conflicting criteria and complex correlation between design parameters.
Satoru Hiwa   +2 more
doaj   +1 more source

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