March 24, 2015 – Mission controllers at NASA’s Jet Propulsion Laboratory in Pasadena, California, have commanded the 20-foot (6-meter) reflector antenna on NASA’s new Soil Moisture Active Passive (SMAP) observatory to begin spinning for the first time. The partial spin-up is a key step in commissioning the satellite in preparation for science operations.
Last week, mission controllers sent commands to release the locking mechanism that prevented the observatory’s spun instrument assembly — the part that spins — from rotating during launch and deployment of the reflector. The spun instrument assembly includes the spin control electronics, radiometer instrument and reflector antenna.
Yesterday, in the first step of a two-step procedure, the spun instrument assembly was spun up to its initial rate of five revolutions per minute (rpm), a process that took about a minute. Initial data indicate the partial antenna spin-up procedure went as planned.
Because of the large size (mass) of the spun instrument assembly and its relatively rapid angular acceleration during spin-up, SMAP’s spacecraft bus rotated in the opposite direction during this process to balance the angular momentum. It reached a peak rate of up to 11 degrees per second. Once the spun instrument assembly spin rate stabilized at five rpm, the spacecraft’s reaction wheels quickly restored the spacecraft bus to a non-rotating, stable attitude. Onboard flight software then turned the observatory back to its science-gathering orientation, with the spin axis pointing straight down to the ground and SMAP’s solar array pointed toward the sun.
The observatory will remain in its current configuration with the spun instrument assembly rotating at five rpm for about three days to allow ground controllers to assess the observatory’s performance at this spin rate before proceeding to the next step. On March 26, after ground analysis of this first antenna spin-up step is completed, mission controllers plan to increase the antenna’s spin speed to its final rate of approximately 15 rpm.
The partial antenna spin-up follows a series of recent propulsive maneuvers by SMAP’s ground flight operations team to adjust the observatory to its final science orbit for mapping operations.
SMAP launched on a United Launch Alliance Delta II rocket on January 31 on a minimum three-year mission to map global soil moisture and detect whether soils are frozen or thawed. The mission will help scientists understand the links in Earth’s water, energy and carbon cycles; help reduce uncertainties in predicting weather and climate; and enhance our ability to monitor and predict natural hazards such as floods and droughts
When fully spun up and collecting science data, SMAP’s antenna will measure a 620-mile-wide (1,000-kilometer) swath of the ground as it flies above Earth at an altitude of 426 miles (685 kilometers). This will allow SMAP to map the entire globe with high-resolution radar data every two to three days.
SMAP is managed for NASA’s Science Mission Directorate in Washington by the agency’s Jet Propulsion Laboratory (JPL) in Pasadena, California, with instrument hardware and science contributions made by NASA’s Goddard Space Flight Center in Greenbelt, Maryland. JPL is responsible for project management, system engineering, radar instrumentation, mission operations and the ground data system. Goddard is responsible for the radiometer instrument. Both centers collaborate on science data processing and delivery to the Alaska Satellite Facility, in Fairbanks, and the National Snow and Ice Data Center, at the University of Colorado in Boulder, for public distribution and archiving. NASA’s Launch Services Program at the agency’s Kennedy Space Center in Florida is responsible for launch management. JPL is managed for NASA by the California Institute of Technology in Pasadena.