HR: 1340h
AN: G33C-0063    [Abstracts]
TI: Progress in an Interferometric Laser Ranging System for a Follow-On Gravity Mission to GRACE
AU: * Craig, R M
EM: rcraig@ball.com
AF: Ball Aerospace & Technologies Corp., 1600 Commerce St., Boulder, CO 80301 United States
AU: Stephens, M
EM: mstephen@ball.com
AF: Ball Aerospace & Technologies Corp., 1600 Commerce St., Boulder, CO 80301 United States
AU: Leitch, J
EM: jleitch@ball.com
AF: Ball Aerospace & Technologies Corp., 1600 Commerce St., Boulder, CO 80301 United States
AU: Pierce, R
EM: rpierce@ball.com
AF: Ball Aerospace & Technologies Corp., 1600 Commerce St., Boulder, CO 80301 United States
AU: Nerem, R S
EM: nerem@colorado.edu
AF: University of Colorado, Campus Box 431, Bpulder, CO 80309 United States
AU: Bender, P
EM: peter.bender@colorado.edu
AF: University of Colorado, Campus Box 431, Bpulder, CO 80309 United States
AU: Folkner, W
G33C-0063 AF: Jet Propulsion Laboratory, 4800 Oak Grove Dr., Pasadena, CO 91109 United States
AU: Watkins, M
G33C-0063 AF: Jet Propulsion Laboratory, 4800 Oak Grove Dr., Pasadena, CO 91109 United States
AB: The Gravity Recovery and Climate Experiment (GRACE) has ushered in a new era for satellite measurements of the Earth system. GRACE provides monthly estimates of the time-varying gravity field, which are largely due to the redistribution of water mass in the Earth system, with a spatial resolution of ~500 km and an accuracy of 1 cm equivalent water. This is accomplished via a suite of instruments including a microwave ranging system, precision accelerometers for measuring non-gravitational forces, and a GPS navigation system. These tremendous advances made by GRACE have led to an interest in launching a follow-on mission with even better performance. The spatial resolution can be improved by improving the ranging performance, implementing a drag-free control system, and flying at a lower altitude. This presentation will focus on our ongoing effort to develop an interferometric laser ranging system that has demonstrated performance near the 1 nm/sec level or better over 5 second intervals, which when coupled with other mission improvements, would improve the spatial resolution to ~100 km for 1 cm water equivalent accuracy. We report progress towards building an engineering model of the instrument, with which we will demonstrate its accuracy in the laboratory over the next few years. The laser system will range directly to the proof masses of the drag-free system, eliminating many of the difficulties associated with post-processing the accelerometer data on GRACE. In addition, we will show new results from our successful laboratory tests of the breadboard design in both ambient and vacuum conditions.
DE: 1200 GEODESY AND GRAVITY
DE: 1219 Gravity anomalies and Earth structure (0920, 7205, 7240)
DE: 1222 Ocean monitoring with geodetic techniques (1225, 1641, 3010, 4532, 4556, 4560, 6959)
DE: 1241 Satellite geodesy: technical issues (6994, 7969)
DE: 1294 Instruments and techniques
SC: Geodesy [G]
MN: Fall Meeting 2005