Thermofluiddynamics of Optimized Rocket Propulsions
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Published By Birkhäuser Basel

9783034899277, 9783034891509

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Classical Gas Dynamics of the ICP

Thermofluiddynamics of Optimized Rocket Propulsions ◽

10.1007/978-3-0348-9150-9_4 ◽

1989 ◽

pp. 32-50

Author(s):

D. Straub

Keyword(s):

Gas Dynamics ◽

Classical Gas

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Description of the Problem

Thermofluiddynamics of Optimized Rocket Propulsions ◽

10.1007/978-3-0348-9150-9_2 ◽

1989 ◽

pp. 13-22

Author(s):

D. Straub

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Test of the MM with Data from LH-LOX Rocket Engies

Thermofluiddynamics of Optimized Rocket Propulsions ◽

10.1007/978-3-0348-9150-9_10 ◽

1989 ◽

pp. 182-211

Author(s):

D. Straub

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Definition of an Ideal Comparative Process

Thermofluiddynamics of Optimized Rocket Propulsions ◽

10.1007/978-3-0348-9150-9_3 ◽

1989 ◽

pp. 23-31

Author(s):

D. Straub

Keyword(s):

Definition Of

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Problems with the NASA-Method

Thermofluiddynamics of Optimized Rocket Propulsions ◽

10.1007/978-3-0348-9150-9_7 ◽

1989 ◽

pp. 65-100

Author(s):

D. Straub

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The Munich Method

Thermofluiddynamics of Optimized Rocket Propulsions ◽

10.1007/978-3-0348-9150-9_9 ◽

1989 ◽

pp. 133-181

Author(s):

D. Straub

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Basic Principles of the Alternative Theory

Thermofluiddynamics of Optimized Rocket Propulsions ◽

10.1007/978-3-0348-9150-9_8 ◽

1989 ◽

pp. 101-132

Author(s):

D. Straub

Keyword(s):

Alternative Theory ◽

Basic Principles

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Summary Part II

Thermofluiddynamics of Optimized Rocket Propulsions ◽

10.1007/978-3-0348-9150-9_11 ◽

1989 ◽

pp. 212-215

Author(s):

D. Straub

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Summary I

Thermofluiddynamics of Optimized Rocket Propulsions ◽

10.1007/978-3-0348-9150-9_6 ◽

1989 ◽

pp. 63-63

Author(s):

D. Straub

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Design Criteria for Rocket Engines

Thermofluiddynamics of Optimized Rocket Propulsions ◽

10.1007/978-3-0348-9150-9_5 ◽

1989 ◽

pp. 51-62

Author(s):

D. Straub

Keyword(s):

Design Criteria ◽

Rocket Engines

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Thermofluiddynamics of Optimized Rocket PropulsionsLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By Birkhäuser Basel

Classical Gas Dynamics of the ICP

Description of the Problem

Test of the MM with Data from LH-LOX Rocket Engies

Definition of an Ideal Comparative Process

Problems with the NASA-Method

The Munich Method

Basic Principles of the Alternative Theory

Summary Part II

Summary I

Design Criteria for Rocket Engines

Thermofluiddynamics of Optimized Rocket Propulsions
Latest Publications