Author:
Leary James C.,Conde Richard F.,Dakermanji George,Engelbrecht Carl S.,Ercol Carl J.,Fielhauer Karl B.,Grant David G.,Hartka Theodore J.,Hill Tracy A.,Jaskulek Stephen E.,Mirantes Mary A.,Mosher Larry E.,Paul Michael V.,Persons David F.,Rodberg Elliot H.,Srinivasan Dipak K.,Vaughan Robin M.,Wiley Samuel R.
Reference26 articles.
1. R.F. Conde et al., Benefits and lessons learned from the use of the compact PCI standard for spacecraft avionics, in 21st Digital Avionics Systems Conference, Paper 9B5, 11 pp., Irvine, CA, 2002
2. G. Dakermanji, C. Person, J. Jenkins, L. Kennedy, D. Temkin, The MESSENGER spacecraft power system design and early mission performance, in Proceedings of the Seventh European Space Power Conference, Special Publication SP-589 (European Space Agency, Noordwijk, 2005), CD-ROM
3. C.J. Ercol, A.G. Santo, Determination of optimum thermal phase angles at Mercury perihelion for an orbiting spacecraft, in 29th International Conference on Environmental Systems, Society of Automotive Engineers, Tech. Paper Ser., 1999-01-21123,10 pp., Denver, CO, 1999
4. C.J. Ercol, J.E. Jenkins, G. Dakermanji, A.G. Santo, L.S. Mason, Prototype solar panel development and testing for a Mercury orbiter spacecraft, in 35th Intersociety Energy Conversion Engineering Conference, American Institute of Aeronautics and Astronautics, Paper AIAA-2000-2881, 11 pp., Las Vegas, NV, 2000
5. R.E. Gold et al., The MESSENGER mission to Mercury: Scientific payload. Planet. Space Sci. 49, 1467–1479 (2001)