GRACE Mission Design : Impact of Uncertainties in Disturbance Environment and Satellite Force Models

Author:: Seywald, Hans
Published:: [2000].
Physical Description:: 1 electronic document
Additional Creators:: Qu, Min, Mazanek, Daniel D., and Kumar, Renjith R.

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Summary:

The Gravity Recovery and Climate Experiment (GRACE) primary mission will be performed by making measurements of the inter-satellite range change between two co-planar, low altitude, near-polar orbiting satellites. Understanding the uncertainties in the disturbance environment, particularly the aerodynamic drag and torques, is critical in several mission areas. These include an accurate estimate of the spacecraft orbital lifetime, evaluation of spacecraft attitude control requirements, and estimation of the orbital maintenance maneuver frequency necessitated by differences in the drag forces acting on both satellites. The FREEMOL simulation software has been developed and utilized to analyze and suggest design modifications to the GRACE spacecraft. Aerodynamic accommodation bounding analyses were performed and worst-case envelopes were obtained for the aerodynamic torques and the differential ballistic coefficients between the leading and trailing GRACE spacecraft. These analyses demonstrate how spacecraft aerodynamic design and analysis can benefit from a better understanding of spacecraft surface accommodation properties, and the implications for mission design constraints such as formation spacing control.

Other Subject(s):

Astronautics (General)

Collection:

NASA Technical Reports Server (NTRS) Collection.

Note:

Document ID: 20000032918.
AAS Paper 00-163.
Space Flight Mechanics Meeting; 23-26 Jan. 2000; Clearwater, FL; United States.

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