HISTORY - Page 8
each. Additionally, six small nozzles would be
installed to provide spatial attitude control in pitch,
yaw, and roll. The gimbaled engines also served to
assist in correcting the same problems, and the swivel
would be hydraulically activated
10
.
The June and July proposals orally presented by Dr.
Wernher von Braun, chief of the Redstone
development team, before the Armed Services Policy
Council began to interest officials at the high
Washington level. Secretary of Defense Charles E.
Wilson designated Reuben B. Robertson of DOD to
investigate the IRBM field. Then, OCRD requested
OCO to compile a list of facts favoring development of
the1,500-mile missile at Redstone. OCO quickly
complied, listing many of the reasons that had been
included in past studies, that is, facilities, competent
personnel, and proven components that could be
redesigned. One new feature was added: that the
REDSTONE missile had been transferred to a
production contractor. This meant that an industrial
capability would be available when the 1,500-missile
reached that stage, an important point to be
considered
11
.
By August 1955, the matter had reached a cost study
stage. In this respect, the Army Chief of Staff
requested an estimate for developing a 1,500-mile
missile at Redstone. 0C0 placed the cost of a six-year
development program at $240 million, but OCRD
believed this to be too conservative and estimated
that the costs would run between $400 and $500
million. Redstone's plans as of September indicated
that the time frame of the development would be
somewhat telescoped, giving an Ordnance Readiness
Date of
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10. RSA OML Study, 1 Jul 55, subj: OML Prop for a Ball GM Sys of 1,500 NM Range, pp. 14-16, Hist Off files.
11. ABMA Ref Book, Part I, JUP, Tab A-4.