The Terra spacecraft supports the operation of
the five instruments on the mission. All instruments
are mounted on the nadir-facing deck of the
spacecraft for a clear view of the Earth.
To support the cooling requirements of ASTER and
MOPITT, the spacecraft provides an advanced
technology capillary-pumped heat transport system that
transports heat from the instruments to the passive
radiators mounted on the spacecraft. This advanced
heat transport system, developed at NASA's Goddard
Space Flight Center, was tested on the Space Shuttle
and is expected to yield significant benefits to this
and future spacecraft.
The science data generated by each instrument are
sent to the spacecraft over high-bandwidth
communication lines. These data are multiplexed and recorded
in a solid-state recorder, then sent to the
communication subsystem for transmission to the ground. This
state-of-art solid-state recorder is designed to hold
approximately two orbits of data, up to 140
Gigabytes, using advanced technology solid-state
memory devices.
For transmission to the ground, two communications
capabilities will be available. First, data can be
transmitted via the Tracking and Data Relay Satellite
System (TDRSS) on Ku band to the TDRSS Ground
Station, White Sands, NM. Second, data can be
transmitted directly to the ground on X band. In both
cases, transmission is scheduled to occur at specific
times based on the availability of TDRSS, or the
proximity of a ground station. Continuous direct
broadcast of MODIS data will be available on X band and
can be received by individual users around the world.
The orientation of the spacecraft is maintained by the
guidance, navigation, and control subsystem. This
complex and precise subsystem maintains spacecraft
pointing accuracy to within 150 arc-seconds of the
desired pointing direction, and determines pointing
to within 90 arc-seconds using star trackers.
Additionally, this subsystem provides safe hold
control in the event of a spacecraft operational anomaly.
Electrical power to operate all the instruments and
spacecraft subsystems is provided by the electrical
subsystem. Power is generated by an advanced,
light-weight solar array using gallium arsenide solar cells.
This power is then converted into operating voltages,
regulated, and distributed to all subsystems and
instruments. Electrical energy is stored in nickel
hydrogen batteries to enable the spacecraft to operate
on the dark portion of the orbit.