Preliminary outline of a liquid rocket propulsion in which the acceleration of the flying Missile is utilized to secure an increase of feeding resulting in a sufficiently strong combustion-unit-pressure (thrust). Outline related to project "Wasserfall"
File — Box: 35, Folder: FE 767
Dates
- Creation: 1920 - 1970
Extent
From the Collection: 100 Linear feet
Language of Materials
From the Collection: German
General
German Translation: Vorläufiger Entwurf eines Flüssigkeitsraketenantriebs, bei dem die Beschleunigung der fliegenden Rakete genutzt wird, um eine Erhöhung der Zufuhr sicherzustellen, was zu einem ausreichend starken Verbrennungseinheitsdruck (Schub) führt. Skizze zum Projekt „Wasserfall“
Author/Editor: N/A
Repository Details
Part of the The University of Alabama in Huntsville Archives & Special Collections Repository
Contact:
M. Louis Salmon Library
301 Sparkman Drive
Huntsville Alabama 35899 United States of America
256-824-6523
archives@uah.edu
M. Louis Salmon Library
301 Sparkman Drive
Huntsville Alabama 35899 United States of America
256-824-6523
archives@uah.edu