30 June 1961 - The Black Vault
30 June 1961 - The Black Vault
30 June 1961 - The Black Vault
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In mid-Apr'11 19S3~<br />
the Aer'ojet General Cor'poratlon,<br />
Cor!solldated .....lJ.ltee Aircraft Corporation (later the Convair<br />
Dlv1sj,on J General Dynamics Corpor-atlon)~ Nor·th American Aviation,<br />
the WADe F1ghter and Bombardment Section and Power Plan~<br />
laboratoryj<br />
and the AFFTC reached agreement that the only meal)S or conducting<br />
the vast ATLAS test program within schedule limitations<br />
and on limited facilIties of the AFFTC Rocket Branch was nru::! tlple<br />
util:tzatlon of test .stands initially. This would be accomplished<br />
by establishing additional test locations on Test Stands 1-3 ar:.d<br />
1_5. 16<br />
!n 1954, a new side test position (1-3B) was added to Te~· t<br />
stand 1-3 by the Apex Steel corporat10n. 17<br />
F1rst Rocketdyne<br />
hot firing of the ATLAS single engine test vehicle f'er- research<br />
and development was performed 10 November 1954.18<br />
pr·e11m.1nary a ttempts J<br />
ATLAS test underway.<br />
accomplish the task properly.<br />
<strong>The</strong>se were<br />
however, only to get the Convair built<br />
Several new test stands would be needed to<br />
<strong>The</strong> new stands would become Test<br />
Stand I-A, 1-1, 1-2, and 1-4 and control station 1-6, all U!1ci.er<br />
study and deotgn in 1953 and 1954.<br />
Test Stand 1-A was fo'reroost of the new facl11 ties. With<br />
1,000 1<br />
000 pound thrust capacity, Test Stand 1-A was the first<br />
stand ever des1gned to acco~~date<br />
a complete lntercontinental<br />
ballistic missile (IC~~). Final drawings and specificat1on~ WGr~<br />
16. H~st of the Rocket BrancnJ Apr 1953 .<br />
17. MIst of Hie Rocket Branch, Oc't 1954.<br />
18. J{lst of- the A~FTG, Jan- Jun 1957, p. 192.<br />
..