It has been awhile since I posted anything to this site. The launch of OSIRIS-REx was such an amazing, emotional experience; it took me about a month to come back down to Earth (pun intended). I have now settled into a normal work routine in Tucson and the team has been busy operating the spacecraft and planning for the encounter with Bennu in 2018. We are now in the Outbound Cruise phase of the mission.
Animation showing the nominal trajectory of OSIRIS-REx from launch through Bennu encounter.
We Have a Healthy Spacecraft
Outbound Cruise began soon after the spacecraft separated from the Atlas V launch vehicle as planned. The spacecraft post-separation activities were all nominal and the spacecraft quickly transitioned to the “Outbound Cruise” operating mode. I studied the separation video quite a bit and noticed what appeared to be a plume originating from the lower portion of the spacecraft. After talking with the spacecraft engineers, we realized that the out-gassing was the result of the initialization of the propulsion system. This out-gassing was also evident in the DSN tracking data since we could see small forces slightly changing the spacecraft trajectory.
Video from the Atlas V DAVIS camera system. The view is from the Centaur upper stage and captures the deployment of the OSIRIS-REx spacecraft.
After launch-vehicle separation, the spacecraft was placed into the “Sun point” attitude (+X spacecraft axis toward the sun) with the solar arrays off-pointed from the sun by 45 degrees. This attitude ensures that the spacecraft will collect sufficient power to remain power positive at all times while keeping the other components from experiencing direct solar heating.
Propulsion System Performance
The propulsion system has been performing well. Momentum dumps using the Attitude Control System (ACS) thrusters are occurring as planned. During these maneuvers, reaction wheel momentum is unloaded by firing the ACS thrusters. Reaction wheels are flywheels that use electric motors to change their rotation speed. As the wheels rotate, the spacecraft counter-rotates as a result of the conservation of angular momentum. Wheel speeds are generally maintained below 3000 RPM which requires desaturation of the built-up angular momentum approximately once every seven days.
We also executed our first Trajectory Correction Maneuver (TCM-1) using the TCM thrusters. This maneuver was placed into the mission plan to clean up any errors introduced by the Atlas V launch vehicle. However, since the Atlas V performance was nearly perfect, we re-designed TCM-1 as a minimal engineering burn, just to check out the TCM thruster performance. Our first major maneuver using the spacecraft main engines is Deep Space Maneuver #1 (DSM-1), which will be executed on December 28th, 2016. The preliminary design cycle for this maneuver has begun, with a DSM-1 Readiness Review planned for December 1st.
Science Instrument Checkouts
As part of checking out the flight system, we turned on all of the science instruments and ran them through some basic functional check outs. I am happy to report that OCAMS, OVIRS, OTES, OLA, and REXIS all completed post-launch aliveness checkouts with no major issues. OCAMS is investigating stray light effects which appear to be due to sunlight reflecting off PolyCam and OTES protruding from the +Z deck. We don’t expect this stray light to be an issue in operations but we are building a detailed optical model of the science deck and planning a follow-on characterization campaign later in Outbound Cruise. This model will allow us to maximize the science value of our imaging campaigns and ensure that stray light does not degrade our science data.
Movie showing the images from MapCam zooming into PolyCam during the OCAMS checkout in Outbound Cruise.
We also switched on the Touch and Go Camera System (TAGCAMS) and successfully acquired 19 images of star fields and spacecraft hardware. TAGCAMS is not part of the science payload; it is considered a component of the spacecraft Guidance, Navigation, and Control system. The purpose of TAGCAMS is to provide imagery during the mission to facilitate navigation to the target asteroid, acquisition of the asteroid sample and confirmation of asteroid sample stowage. The cameras were designed and built by Malin Space Science Systems (MSSS) based on requirements developed by Lockheed Martin and the OSIRIS-REx project.
We still have many activities planned for Outbound Cruise. We will perform a thorough instrument calibration campaign at Launch + 6 months. We are busy planning for an extensive instrument check out and characterization during the Earth Gravity Assist in September 2017. We also have some tricks up our sleeves, with a science observing campaign planned for February 2017. Stay tuned for more details about this exciting activity in future blog posts.
Overall, the launch and early checkout of the OSIRIS-REx flight system has gone flawlessly. We have an amazing spacecraft and an extremely talented operations team. There is a lot of work to do to get ready for the encounter with Bennu in August 2018. However, we have the right equipment and the right team to get this job done successfully. With sample acquisition nominally scheduled for July 2020, OSIRIS-REx promises to be a highlight of planetary exploration over the next four years.