Box 27
Container
Contains 113 Results:
Roll of missile V2 about its longitudinal axis immediately after take-off due to lateral wind (SAM Steering Control Machine operating without gyros)., 1939-06-29
File — Box: 27, Folder: Arch 86/6 (Translation)
Dates:
1939-06-29
Steering Control without vane return, 1939-07-04
File — Box: 27, Folder: Arch 86/7 (Translation)
Dates:
1939-07-04
Calculation of the behavior of the steering machine designed by the Kreiselgeraete Company, 1939-10-20
File — Box: 27, Folder: Arch 86/11 (Translation)
Dates:
1939-10-20
A contribution to the theory of airplane steering control, 1941-02-06
Fonds — Box: 27, Folder: Arch 86/69
Dates:
1941-02-06
Summary of reports on the theory of steering machines with linear steering control equations and the stability of motion about the center of gravity, 1942-04-01
File — Box: 27, Folder: Arch 86/102
Dates:
1942-04-01
Stress on the missile caused by air resistance during reeentry into atmosphere: Part II, 1942-05-07
File — Box: 27, Folder: Arch 86/103
Dates:
1942-05-07
Study of the LGW (Formally SAM) Steering Machine Type K 12 with Non-Idealized Characteristics, 1946-02-15
File — Box: 27, Folder: Arch 86/104
Dates:
1946-02-15
Mixing Ratios for Lateral Guide Beam Control of the Missile A4, 1942-07-01
File — Box: 27, Folder: Arch 86/106
Dates:
1942-07-01
On the Application of the Theory of the Loci to Steering Control Problems, 1942-08-21
File — Box: 27, Folder: Arch 86/107
Dates:
1942-08-21