This directory contains long-term predict MGS trajectory SPKs overlapping MER surface operations time interval: spk_031201-040401_020415.bsp spk_040401-040801_020416.bsp spk_040801-050101_020416.bsp They have been created by MGS NAV in July 2002. The release form that accompanied these files is provided at the end of this file. Note that these SPKs were initially released for the s/c ID -95 (MGS SIM). This ID has been replaced by the s/c ID -94 (MGS OPS) in October 18, 2002. Contact Boris Semenov, NAIF (4-8136) or Stuart Demcak, MGS NAV (x3-7961) if you have any questions regarding these files. ------------------------------------------------------------------- MSOP FILE RELEASE FORM Mission Name: MARS_GLOBAL_SURVEYOR Spacecraft Name: MARS_GLOBAL_SURVEYOR_SIM File Name: optg_030701-040301_020415 File Type: OPTG File Creation Time: 2002-105T18:09:22 DOM Store Time: 2002-200T22:25:43 File Start Time: 2003-182T00:00:00.000 File Stop Time: 2004-092T01:00:00.000 File Name: optg_040301-050101_020416 File Type: OPTG File Creation Time: 2002-106T12:03:06 DOM Store Time: 2002-200T22:26:08 File Start Time: 2004-092T00:00:00.000 File Stop Time: 2005-001T01:00:00.000 File Name: spk_031201-040401_020415 File Type: MO-M-SPICE-6-SPK-V1.0 File Creation Time: 2002-200T16:00:00 DOM Store Time: 2002-203T14:35:20 File Start Time: 2003-12-01T00:00:00.000 File Stop Time: 2004-04-01T01:00:00.000 File Name: spk_040401-040801_020416 File Type: MO-M-SPICE-6-SPK-V1.0 File Creation Time: 2002-200T16:03:58 DOM Store Time: 2002-203T14:36:49 File Start Time: 2004-04-01T00:00:00.000 File Stop Time: 2004-08-01T01:00:00.000 File Name: spk_040801-050101_020416 File Type: MO-M-SPICE-6-SPK-V1.0 File Creation Time: 2002-200T16:09:21 DOM Store Time: 2002-203T14:38:24 File Start Time: 2004-08-01T00:00:00.000 File Stop Time: 2005-01-01T01:00:00.000 Notes: ~~~~ These files should be used for planning purposes only. They should NOT be used for MGS flight operations. The S/C ID is 95. These files are extensions of the 4/12/2002 6 month MGS delivery. No OSM maneuvers (for MER synchronization) were included. An acceleration of 0.10e-10 km/s^2 was used to simulate predicted AMD events. Note that NAV has made its best attempt to model the future AMD effects and C-mode occurances. However, future AMDs can be quite different than the predictions. So the predicted trajectory will be subject to these perturbations and/or uncertainties. Prepared by: Stuart Demcak Mon Jul 22 07:49:23 PDT 2002 Approval: Pat Esposito