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Rocket propulsion optimisation and non-optimum losses: various maxima and non-linear scaling

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posted on 2020-10-15, 11:49 authored by Dennis Carton
Rocket propulsion optimisation and non-optimum losses: various maxima and non linear scaling

History

School

  • Aeronautical, Automotive, Chemical and Materials Engineering

Department

  • Aeronautical and Automotive Engineering

Publisher

Loughborough University of Technology

Rights holder

© Dennis Carton

Publication date

1968

Notes

A Master's Thesis. Submitted in partial fulfilment of the requirements for the award of the degree of Master of Science of Loughborough University of Technology.

Language

  • en

Supervisor(s)

Peter Sharman

Qualification name

  • MSc

Qualification level

  • Masters

Usage metrics

    Aeronautical and Automotive Engineering Theses

    Categories

    Keywords

    Rocket propulsionEngineering not elsewhere classified

    Licence

    CC BY-NC 4.0

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