Box 25
Container
Contains 91 Results:
Part lists and blue prints to report # 55/2a. Description of and working directions for the measurement device for the 25 ton combustion unit, 1941-12-20
File — Box: 25, Folder: Arch 55/2a (Copy)
Dates:
1941-12-20
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:
1948-08
Report on air pressurization of fuel tanks, 1941-07-05
File — Box: 25, Folder: Arch 56/3
Dates:
1941-07-05
Report on air pressurization of fuel tanks, 1941-07-05
File — Box: 25, Folder: Arch 56/3 (Copy)
Dates:
1941-07-05
Report on missiles using Nitric acid as propellant, 1941-11-20
File — Box: 25, Folder: Arch 56/4 (Translation)
Dates:
1941-11-20
Report on the design and static test of the brake flap device for missile A5 III, 1941-08-07
File — Box: 25, Folder: Arch 56/5 (Translation)
Dates:
1941-08-07
Tail unit equation in the Vickers "Wellington." Investigation of Motion, 1941-08-14
File — Box: 25, Folder: Arch 56/6
Dates:
1941-08-14
Missile A4: Variation of pressure in the alcohol; pump inlet pressure; pressure on top and hose of tanks; supporting forces of the tank.
File — Box: 25, Folder: Arch 56/7
Dates:
1920 - 1970
Investigation of the variation of pressure inside the missile. Protection of thin sheeted alcohol tank during descent., 1948-08
File — Box: 25, Folder: Arch 56/8
Dates:
1948-08
Calculations of steam consumption and additional thrust provided by steam exhaust nozzles for the first launching, 1942-01-26
File — Box: 25, Folder: Arch 56/10
Dates:
1942-01-26