The telescope's primary reflecting mirrors are a pair of
Gregorian dishes (facing opposite directions), that focus the signal onto a pair of secondary reflecting mirrors. They are shaped for optimal performance: a
carbon fibre shell upon a Korex core, thinly-coated with aluminium and
silicon oxide. The secondary reflectors transmit the signals to the corrugated feedhorns that sit on a
focal plane array box beneath the primary reflectors. The receivers are
polarization-sensitive differential
radiometers measuring the difference between two telescope beams. The signal is amplified with
High-electron-mobility transistor (HEMT)
low-noise amplifiers, built by the
National Radio Astronomy Observatory (NRAO). There are 20 feeds, 10 in each direction, from which a radiometer collects a signal; the measure is the difference in the sky signal from opposite directions. The directional separation
azimuth is 180°; the total angle is 141°. To improve subtraction of foreground signals from our
Milky Way galaxy, the WMAP used five discrete radio frequency bands, from 23 GHz to 94 GHz. The WMAP's base is a -diameter
solar panel array that keeps the instruments in shadow during CMB observations, (by keeping the craft constantly angled at 22°, relative to the
Sun). Upon the array sit a bottom deck (supporting the warm components) and a top deck. The telescope's cold components: the focal-plane array and the mirrors, are separated from the warm components with a cylindrical, -long thermal isolation shell atop the deck. Passive thermal radiators cool the WMAP to approximately ; they are connected to the
low-noise amplifiers. The telescope consumes 419 W of power. The available telescope heaters are emergency-survival heaters, and there is a transmitter heater, used to warm them when off. The WMAP spacecraft's temperature is monitored with
platinum resistance thermometers. The WMAP's calibration is effected with the CMB dipole and measurements of
Jupiter; the beam patterns are measured against Jupiter. The telescope's data are relayed daily via a 2-GHz
transponder providing a 667
kbit/s downlink to a
Deep Space Network station. The spacecraft has two transponders, one a redundant backup; they are minimally active – about 40 minutes daily – to minimize
radio frequency interference. The telescope's position is maintained, in its three axes, with three
reaction wheels,
gyroscopes, two
star trackers and
Sun sensors, and is steered with eight
hydrazine thrusters. == Launch, trajectory, and orbit ==