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Comparative calculations of the design parameters and for missile A4 based on the use of new propellents. (Nitric - acid and diesel oil), 1948-08

 File — Box: 25, Folder: Arch 56/1

Dates

  • Creation: 1948-08

Extent

From the Collection: 100 Linear feet

Language of Materials

From the Collection: German

General

German Translation: Vergleichende Berechnungen der Designparameter und für den Flugkörper A4 auf Basis des Einsatzes neuer Treibstoffe. (Salpetersäure und Dieselöl)

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