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Thermofluiddynamics of optimized rocket propulsions extended Lewis code fundamentals

Author: Dieter Straub
Publisher: Basel ; Boston : Birkhäuser Verlag, 1989.
Edition/Format:   Print book : EnglishView all editions and formats
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Additional Physical Format: Online version:
Straub, Dieter, 1934-
Thermofluiddynamics of optimized rocket propulsions extended Lewis code fundamentals.
Basel ; Boston : Birkhäuser Verlag, 1989
(OCoLC)555697845
Online version:
Straub, Dieter, 1934-
Thermofluiddynamics of optimized rocket propulsions extended Lewis code fundamentals.
Basel ; Boston : Birkhäuser Verlag, 1989
(OCoLC)608482504
Document Type: Book
All Authors / Contributors: Dieter Straub
ISBN: 3764323140 9783764323141 0817623140 9780817623142
OCLC Number: 19352566
Description: 265 pages : illustrations ; 23 cm
Contents: Part One: Optimal comparative process for rocket engines. 1. Description of the problem --
Definitiion of an ideal comparative process --
3. Classical gas dynamics of the ICP --
4. Design criteria for rocket engines --
Summary I. Part Two: Thermofluiddynamics of rocket propulsion. 1. Problems with the NASA-methods --
2. Basic principles of the alternative theory --
3. The Munich method --
4. Test of the MM with data from LH-LOX rocket engines --
5. Summary part II.
Responsibility: Dieter Straub ; [translated from the German by C.W. Offermann].

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