The first step in an attempt at animal verification of the adequacy of
the Mercury flight program was the development of two tests by NASA in
collaboration with the U.S. Air Force School of Aviation Medicine in
which there would be a biomedical evaluation of the accelerations
experienced during the abort of a Mercury flight at and shortly after
liftoff. These flights were launched at the NASA Wallops Station with a
Little Joe solid-fuel launch vehicle.
Two Little Joe launches were made with activation of the escape rockets
during the boost phase to secure maximum acceleration; only a brief
period of weightlessness was attained. The first launch was on December
4, 1959, and the other on January 21, 1960. A 36 by 18-inch sealed,
125-pound, cylindrical capsule containing the subject, an 8-pound
_Macaca mulatta_, the necessary life-support system, and associated
instrumentation was flown in a "boilerplate" model of the Mercury
spacecraft. The rhesus monkeys were named "Sam" and "Miss Sam."
The flight profile included maximum accelerations of about 10 to 12 g
and periods of about 3 minutes at 0±0.02 g. The peak altitude obtained
in the last ballistic flight was about 280 000 feet. The experimental
capsule was pressurized at 1 atmosphere with 100 percent oxygen at the
start of the experiment and fell to just below a half atmosphere of
oxygen due to breathing during flight. The capsule temperature was kept
between 10° and 20° C in both flights.
The measurements taken from the rhesus monkeys were the
electrocardiogram, respiration, body temperature, eye movements, and bar
pressing, but only partial results were obtained in the first flight.
Oxygen tension, total pressure, capsule temperature, and relative
humidity were recorded. Both animals were recovered alive and did not
show pathologic alterations in their physiologic and psychological
reactions.