Box 25
Container
Contains 91 Results:
Reel-C 2075 A.T.I. 22148 RESTRICTED On the relations of combustion chamber pressure, throughout, thrust and mixture proportions for the 25-ton and 8-ton stages, 1944-10
File — Box: 25, Folder: Arch 57/12
Dates:
1944-10
Reel-C 3124B A.T.I. 65085 RESTRICTED This translation was made for the Air Materiel Command as part of: Contract No. W33-038-ac-14191 Project MX-770 Operating Data of the German A4 Missile, 1942-02-11
File — Box: 25, Folder: Arch 57/15
Dates:
1942-02-11
Reel-C 1373 A.T.I. 32544 RESTRICTED The accuracy of synchronization of the combustion unit without conducting combustion tests, 1944-09
File — Box: 25, Folder: Arch 57/22
Dates:
1944-09
Investigations on decrease of high - pressure nitrogen during the combustion test. (Experimental zisilles with mass produced turbo - pumps), 1943-05-14
File — Box: 25, Folder: Arch 57/6g
Dates:
1943-05-14
Investigations on decrease of high - pressure nitrogen during the combustion test. (Experimental zisilles with mass produced turbo - pumps), 1943-05-14
File — Box: 25, Folder: Arch 57/6g (Translation)
Dates:
1943-05-14
Simplified method of synchronization report 1: preliminary synchronization, 1943-12-28
File — Box: 25, Folder: Arch 57/8
Dates:
1943-12-28
Developments and investigations on the A-4 combustion cut-off problem, 1943-07-23
File — Box: 25, Folder: Arch 57/9
Dates:
1943-07-23
The adiabatic exponent k for calculation of thrust on ground and during flight concering the german A4 missile, 1943-10-13
File — Box: 25, Folder: Arch 57/11
Dates:
1943-10-13
Simplified method of synchronization Report 2: synchronization according to injection and combustion tests, 1944-01-18
File — Box: 25, Folder: Arch 57/13
Dates:
1944-01-18
Influence of the time of delay upon the range, 1944-02-18
File — Box: 25, Folder: Arch 57/17
Dates:
1944-02-18