Mars Global Surveyor Flight Status Report Tuesday, 22 September 1998 At 11:00 a.m. PDT on Wednesday this week, Surveyor's onboard computer will execute a maneuver command sequence to initiate aerobraking. This 12-second firing of the spacecraft's main rocket engine will take place near the high point of orbit #573. The effect of the burn will be a drop in the low point of Surveyor's orbit from its current altitude of 106.5 miles (171.4 km) down into the upper fringes of the Martian atmosphere at 79 miles (127 km). About 7.5 hours after the burn, Surveyor will reach the low point of its orbit and will encounter the atmosphere for the first time since March of this year. For the next five months, Surveyor will repeatedly fly through the upper Martian atmosphere and use air resistance to gradually shrink the size of the orbit. The goal is to reduce the period from its current value of 11.6 hours to just under two hours. Global mapping operations from this two-hour orbit are scheduled to begin in April of next year. Originally, aerobraking was scheduled to resume on Monday, September 14th. However, two minor delays forced a postponement until tomorrow. The first of the two delays was called to permit the flight team to conduct communication tests over the low-gain antenna. On Wednesday, September 9th, the flight team noted a minor communications irregularity from the receiver on the low-gain antenna. Because this antenna serves as the backup to the primary high-gain antenna in the event of a contingency situation, the flight team prudently delayed the start of aerobraking in order to conduct these tests. After successful tests on the low-gain receiver, aerobraking was rescheduled to start on Thursday, September 17th. Early that morning, the onboard computer's fault-protection routines automatically canceled the command sequence that would have fired the main rocket engine to restart aerobraking. The cancellation of the sequence occurred because the computer detected a low charge level in Surveyor's batteries. This cancellation action was a pre-programmed response designed to keep the spacecraft safe in case of an unexpected event. Further analysis revealed that a minor command sequence processing error resulted in a missed command to move one of Surveyor's two solar panels into its proper position. With one of the two panels out of position, the electrical system was low on solar energy and began to draw power from the batteries to compensate. At this time, software engineers have already remedied the software on the ground that caused the missing command. Over last weekend, Surveyor remained in "contingency mode" to allow the flight team time to recharge the batteries and reset the spacecraft hardware for the start of aerobraking. In this mode, the spacecraft is placed in a safe, Sun-pointed orientation favorable from a power and communications perspective. At 9:00 p.m. on Monday, the flight team commanded the spacecraft back to its normal operational mode with the high-gain antenna pointed at the Earth. Later today, command sequences will be transmitted to the spacecraft to execute the maneuver sequence that will resume aerobraking tomorrow. After a mission elapsed time of 684 days from launch, Surveyor is 213.16 million miles (343.04 million kilometers) from the Earth and in an orbit around Mars with a high point of 11,083 miles (17,836 km), a low point of 106.5 miles (171.4 km), and a period of 11.6 hours. All systems continue to perform as expected. --------------------------------------- Status report prepared by: Office of the Flight Operations Manager Mars Surveyor Operations Project NASA Jet Propulsion Laboratory California Institute of Technology Pasadena, CA 91109 ---------------------------------------