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Key Spacecraft Components

Now that we have an idea how GRACE works, let's peer "under the hood" of this high-tech wonder and understand some of the component parts of GRACE. These components can be seen in the photos on pages 2 and 4; the letters following the name of each component in parentheses correspond to the labels on the diagrams below each photo.

GRACE instrumnents top view

GRACE instruments internal view

The positions of the two GRACE satellites change in response to variations in Earth's gravity field. When the two spacecraft pass over the ocean, the distance between them is unchanged (first panel). But when the lead spacecraft encounters a change in gravity over a denser land mass (second panel), it pulls away from the trailing spacecraft, which is still over water. The lead spacecraft moves back over water (third panel), but now the trailing spacecraft changes position in response to the greater pull of gravity over the land mass.

The drawings are not to scale. In reality, the GRACE satellites are spaced about 220 kilometers apart, and changes in distance between them would be undetectable by human eyes. GRACE has an onboard microwave-ranging system that makes precise, continuous measurements of the distance between the two spacecraft as they orbit the Earth.

K-band Ranging System (KBR). Provides precise (within 10 Ám) measurements of the distance change between the two satellites needed to measure fluctuations in gravity.

Ultra Stable Oscillator (USO). Provides frequency generation for the K-band ranging system.

SuperSTAR Accelorometers (ACC). Precisely measures the non-gravitational accelerations acting on the satellite.

Star Camera Assembly (SCA). Precisely determines the two satellites' orientation by tracking them relative to the position of the stars.

Coarse Earth and Sun Sensor (CES). Provides omnidirectional, reliable, and robust, but fairly coarse, Earth and Sun tracking. Used during initial acquisition and whenever GRACE operates in safe mode.

Center of Mass Trim Assembly (MTA). Precisely measures the offset between the satellite's center of mass and the "acceleration-proof" mass and adjusts center of mass as needed during the flight.

Black-Jack GPS Receiver and Instrument Processing Unit (GPS). Provides digital signal processing; measures the distance change relative to the GPS satellite constellation.

Globalstar Silicon Solar Cell Arrays (GSA). Covers the outer shell of the spacecraft and generates power.

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The GRACE mission is jointly implemented by NASA and DLR under
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Last Modified: Wed Nov 03, 2004
CSR/TSGC Team Web