Box 16
Container
Contains 66 Results:
Report on the coefficient of adhesion of shrunk seats based on the shrunken annular gap nozzles, 1942
File — Box: 16, Folder: 111/03
Dates:
1942
Report on the 25-ton ring-gap mixing nozzle (design A), 1942-05
File — Box: 16, Folder: 111/04
Dates:
1942-05
Catalysts for the decomposition of high-percentage hydrogen peroxide on a ceramic basis, 1944-08-01
File — Box: 16, Folder: 112/01
Dates:
1944-08-01
Investigation of the occurrence of tumbling movements of the A4 when entering the air envelope, 1943-07-16
File — Box: 16, Folder: 113/1
Dates:
1943-07-16
Floor plan of the assembly hall C2 8/45, 1943-03-18
File — Box: 16, Folder: 114/01
Dates:
1943-03-18
Control of the folding arc of the unit with the help of two short-wave transmitters, 1939-10-31
File — Box: 16, Folder: 115/02
Dates:
1939-10-31
Mounting of the A-4 and A-10 missile in a static test stand. Aerodynamic lead in the missile at altitudes between 50 and 100 km., 1939-11-29
File — Box: 16, Folder: 115/03
Dates:
1939-11-29
A flexible mounting of the missile A-4., 1940-05-16
File — Box: 16, Folder: 115/04
Dates:
1940-05-16
Influence of occurring as a restriction of the thrusters. Alignment errors on the A4's trajectory control in the first few seconds after take-off, 1941-06-11
File — Box: 16, Folder: 115/05
Dates:
1941-06-11
On the dependence of the beacon field on the distance between the dipoles and on the phase shift, 1941-09-20
File — Box: 16, Folder: 115/06
Dates:
1941-09-20