ABSTRACT
The Geophysical
Institute has developed a new type of sounding rocket
payload that is expected to fly on a rocket mission launched from Poker Flat
in early 2010. The new payload design is collection of sub-payloads, each of
which is an approximately five-pound, rocket-propelled cylinder that will launch
out of the side of a Terrier-Orion rocket during flight. The ultimate goal
is to achieve the capability to disperse a three-dimensional constellation
of trimethyl-aluminum “puffs” which will allow for the measurement
of three-dimensional neutral wind fields and gradients in the polar lower thermosphere.
A brief summary of the scientific motivation for the
mission and the properties of the polar lower thermosphere will be presented
and preliminary results of Fall 2009 testing of the ampule design will
be shown. The testing results include high speed video (up to 16,000 frames
per second) and other data from test ampule explosions under vacuum, rocket
motor burns at a variety of pressures, and ampule launch trials. Some aspects
of the field of rocket propulsion relevant to these tests will also be
discussed.
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