PDS_VERSION_ID = PDS3 RECORD_TYPE = STREAM LABEL_REVISION_NOTE = "2010-12-08 A.C.Raugh Extracted from 'catalog.lbl' file from PDS1 test volume PHB_1001 and reformatted to current PDS3 standards" OBJECT = MISSION MISSION_NAME = "PHOBOS 2" OBJECT = MISSION_INFORMATION MISSION_START_DATE = 1988-07-07 MISSION_STOP_DATE = 1989-03-27 MISSION_ALIAS_NAME = "PHOBOS" MISSION_DESC = " Mission Overview ================ The spacecraft Phobos 1 and 2 were launched on 7 and 12 July 1988. The mission was to have three stages: investigations of Sun and interplanetary space during the flight from Earth to Mars; studies of both Mars and Phobos during the orbit of the spacecraft around Mars; and studies of Phobos as the spacecraft approached to within 50 m of its surface. Contact with Phobos 1 was lost on 1 September 1988 during the cruise phase; contact was lost with Phobos 2 just before the third stage of the mission. However, valuable data on Mars and Phobos were acquired prior to loss of contact. Mission Phase Information ========================= Phase 1 - Cruise ---------------- Start Time: 1988-07-07 Stop Time: 1989-01-29 Phobos 2 was launched on July 12, 1988. The first correction of the trajectory was made on July 21, 1988. On January 29, 1989, a retarding impulse was applied and Phobos 2 was transferred from Earth-to-Mars trajectory to the elliptical equatorial orbit of a martian artificial satellite. Phase 2 - Mars Orbit -------------------- Start Time: 1989-01-29 Stop Time: 1989-03-27 On January 29, 1989, a retarding impulse was applied and Phobos 2 was transferred from Earth-to-Mars trajectory to the elliptical equatorial orbit of a martian artificial satellite. The spacecraft's orbits were corrected several more times in February, in order to achieve a circular orbit, almost the same as that of Phobos, although somewhat higher. In March, several intermediate corrections transferred the spacecraft into a quasi-synchronous orbit with Phobos. Eventually, the craft was transferred to an orbit closer to Phobos, and then guided closer to Phobos itself. On March 27, 1989, after television imaging of Phobos during which Phobos 2 changed its orientation so that its field of view pointed at Phobos, radio contact was lost." MISSION_OBJECTIVES_SUMMARY = " Mission Objectives Overview =========================== The Phobos spacecraft was to have come as close as ~50 m to Phobos which would have made it possible to obtain high-resolution television images of the surface of Phobos, to study the elemental and mineralogical composition of the regolith, the internal structure of Phobos, and to put landers on the moon's surface. Besides studies of Phobos, and the martian surface, atmosphere and plasma environment of Mars, both of the Phobos spacecraft were to make observations of the Sun and interplanetary space during the flight from Earth to Mars." END_OBJECT = MISSION_INFORMATION OBJECT = MISSION_HOST INSTRUMENT_HOST_ID = "PHB2" OBJECT = MISSION_TARGET TARGET_NAME = "JUPITER" END_OBJECT = MISSION_TARGET OBJECT = MISSION_TARGET TARGET_NAME = "MARS" END_OBJECT = MISSION_TARGET OBJECT = MISSION_TARGET TARGET_NAME = "PHOBOS" END_OBJECT = MISSION_TARGET END_OBJECT = MISSION_HOST OBJECT = MISSION_REFERENCE_INFORMATION REFERENCE_KEY_ID = "PSS1991-01-02" END_OBJECT = MISSION_REFERENCE_INFORMATION OBJECT = MISSION_REFERENCE_INFORMATION REFERENCE_KEY_ID = "SAGDEEV&ZAKHARO1989" END_OBJECT = MISSION_REFERENCE_INFORMATION END_OBJECT = MISSION END