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Research article

First published 2025-10

Numerical geometry optimization of a hybrid rocket engine using finite volume method

Dilara Koçak, Aydoğan Özdamar

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2018-4

Conceptual study of a dual-rocket-based-combined-cycle powered two-stage-to-orbit launch vehicle

Fan Zhang, Huiqiang Zhang, Bing Wang

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2001-4

Testing of a novel propulsion system for micro air vehicles

W S Cheung, J R Tilston

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2014-4

Firing tests of hybrid engine with varying oxidiser nature and operating conditions

Nicolas Gascoin, Alexandre Mangeot, Camille Marin [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

Open access

Research article

First published 2025-1

Trihybrid nanofluid flow through nozzle of a rocket engine: Numerical solution and irreversibility analysis

Basharat Ullah, Rabia Rehman, Hafiz Abdul Wahab [...]

Energy Exploration & Exploitation

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Research article

First published 2018-6

Effects of aramid fibers and colloidal particle fillers in composite ethylene propylene diene monomer rubber thermal insulators for rocket motor insulation

AM El-Dakhakhny, AF Ahmed, M Rutkevičius [...]

Journal of Composite Materials

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Research article

First published 2025-8

A practical method for reliability evaluation of hybrid system under unit life submitted with different distribution

Lili Bai, Lei Tian

Proceedings of the Institution of Mechanical Engineers,Part O: Journal of Risk and Reliability

Search results

Numerical geometry optimization of a hybrid rocket engine using finite volume method

Conceptual study of a dual-rocket-based-combined-cycle powered two-stage-to-orbit launch vehicle

Testing of a novel propulsion system for micro air vehicles

Firing tests of hybrid engine with varying oxidiser nature and operating conditions

Trihybrid nanofluid flow through nozzle of a rocket engine: Numerical solution and irreversibility analysis

Effects of aramid fibers and colloidal particle fillers in composite ethylene propylene diene monomer rubber thermal insulators for rocket motor insulation

A practical method for reliability evaluation of hybrid system under unit life submitted with different distribution