1Dept. of Mechanical Engineering, Brigham Young University, Provo, UT 84602, USA
2Marshall Space Flight Center, NASA, Huntsville, AL 35812, USA
Received: 10 Apr 2013 – Revised: 11 Jun 2013 – Accepted: 01 Jul 2013 – Published: 02 Dec 2013
Abstract. This paper describes the conception, modeling, and development of a fully compliant two-degree-of-freedom pointing mechanism for application in spacecraft thruster, antenna, or solar array systems. The design objectives and the advantages of a compliant solution are briefly discussed. Detailed design decisions to meet project objectives are described. Analytical and numerical models are developed and subsequently verified by prototype testing and measurements in several iterations. A final design of the 3-D printed titanium monolithic pointing mechanism is described in detail and its performance is measured.
Merriam, E. G., Jones, J. E., Magleby, S. P., and Howell, L. L.: Monolithic 2 DOF fully compliant space pointing mechanism, Mech. Sci., 4, 381-390, doi:10.5194/ms-4-381-2013, 2013.