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The MAP spacecraft will probe
conditions in the early universe by measuring the properties of
the cosmic microwave background radiation over the full sky.
MAP will measure fluctuations in the
Cosmic Background Radiation temperature. The information provided
by this detailed map will be used to answer questions about the
origin, content and future of the universe.
The MAP instrument consists of a
set of passively cooled microwave radiometers with 1.4 x 1.6 meter
diameter primary reflectors to provide the desired angular
resolution. The sensitivity of the cosmic microwave background map
will be better than 20 microKelvin (0.000020 Kelvin) per 0.3
degree square pixel. MAP will measure temperature differences on
the sky using symmetric microwave receivers coupled to
back-to-back telescopes. By measuring temperature differences,
rather than absolute temperatures, most spurious signals will
cancel. Five frequency bands from 22 GHz to 90 GHz will allow
emission from the Galaxy and environmental disturbances to be
modeled and removed based on their frequency dependence. The MAP
instrument will be continuously shaded from the Sun, Earth, and
Moon by the spacecraft.
MAP will observe from
a Lissajous orbit about the L2 Sun-Earth Lagrange point 1.5
million km from Earth. The trajectory selected to attain such an
orbit consists of 2.5-3.5 lunar phasings loops followed by a ~100
day cruise to L2. No thruster firings are required to enter the L2
orbit.
The following
animation indicates the path MAP will follow to L2. The trajectory
features 2.5 or 3.5 lunar phasing loops which assist the
spacecraft in reaching L2. The cruise time to L2 is approximately
100 days after the lunar phasing loops are completed. Once in
orbit about L2, the satellite maintains a Lissajous orbit such
that the MAP-Earth vector remains between 1 and 10 degrees off the
Sun-Earth vector to satisfy communications requirements while
avoiding eclipses. Station-keeping maneuvers will be required ~4
times per year to maintain this orbit.

Courtesy NASA GSFC: MAP
Trajectory to L2
MAP will rotate once
every two minutes around
its spin axis, with the aid of three "reaction wheels"
symmetrically placed around the base of the spacecraft. The spin
axis of MAP will maintain a fixed angle of 22.5 degrees with
respect to the Sun-Earth line. This axis will revolve around the
Sun-Earth line every hour, and rotate annually with the Earth
around the Sun. This scan pattern will permit MAP to see any one
point in the sky from many different perspectives.
The NASA Goddard Space
Flight Center, Princeton University, UCLA, and The University of
Chicago are the Science Team institutions that are responsible for
the MAP Project.

MAP
Microwave
Anisotropy
Probe
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SATELLITE
|
| Int'l Designation |
2001-027A
|
Launched
|
| Owner / Sponsor |
NASA
/ Goddard Space Flight Center (GSFC)
|
| Mission |
Science
|
| Satellite Bus |
Goddard
Space Flight Center in partnership with Princeton University
|
Custom
|
| Launch Mass |
840
kg (1850 lbm)
|
| Mission Orbit |
L2
(1-10 degree Lissajous orbit)
Lunar assist with phasing loops
|
| Design Life |
27
months; fuel limit > 3 years
|
| Power (EOL) |
0.419
kW; 3.1 m2 GaAs/Ge array 22.5 degrees off full
Sun
23 A-hr NiH battery; no eclipses
|
|
LAUNCH
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| Launch Vehicle
Model |
Delta
2 7425-10 |
| Launch Date / Time |
2001
June 30
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19:46:46
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|
FINANCIAL
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| Satellite cost |
US$95
million
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| Web Links |
MAP Home Page
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