SNAP TIMELINE
1952 to 1955
The Atomic Energy Commission(AEC)* did an analysis of
nuclear power sources and evaluated them on their feasibility to be used with
future spacecraft.
1954
Specialized studies on nuclear-electric sources for space
applications were done under the Pied Piper Program conducted in 1954(Ref. 2).
These studies were later integrated into the Weapons Systems 117-L (WS 117-L)
program, which conducted studies on a wide spectrum of energy and satellite
systems for space.
1955
A joint AF-AEC committee established specifications for
nuclear power in space. This included the power, life and interrelation of the
nuclear device and spacecraft. The role of the AEC was to promote the
development and utilization of atomic energy. The Pied Piper Program was later
renamed the SNAP program.
A formal request for proposal studies was issued jointly by
the
Department of Reactor Development (DRD) of the AEC and the
Air Force Wright Air Development Center (AFWADC). AiResearch and Atomics
International (AI) proposed a Zr-H reactor coupled to a Mercury-Rankine power
conversion system. The early work was done independently by Lockheed Missiles
and Space Division(LMSD) with Thompson Ramo Wooldridge (TRW) and AI with
AiResearch of the Garrett Corporation. Funding was jointly sponsored by the AEC
for the reactor development and the AF for work on the power conversion system
(Ref. 3).
June 1957
AEC assumed complete control of the project and AI became
the prime contractor. TRW was contracted to complete work on
the power conversion system and the research being completed by AiResearch was
phased out completely by March 1958 (Ref. 3). Atomics International chose an
epithermal reactor design for space applications over a fast reactor because
the critical mass of a useful fast reactor would result in an uranium cost of
the order of one million dollars (1961). For a reactor which was to be produced
in quantity the resulting cost would have been greater than that of delivery
into space when the launch costs fell below $1000 per pound (Ref. 4). Also, for
temperatures between 315 to 10930C the Zr-H reactor was lighter than an
equivalent fast reactor.
October 1957
The first SNAP critical assembly was tested in October 1957,
three weeks after Sputnik I was launched. The SNAP Experimental Reactor (SER)
was operated in 1959 and the SNAP 2 Developmental Reactor (S2DR) in 1961. The
SNAP 2 reactor had Zr-H fuel to be coupled with a Mercury-Rankine power
conversion system. Table 1 is a compilation of SNAP reactor test experience and
Table 2 outlines the development program.
1958
The AF requested Al to study a reactor designed with
thermoelectric
conversion units.
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