Author:
Schock A.,Noravian H.,Or C.,Kumar V.
Reference19 articles.
1. Schock, A., Design evolution and verification of the general-purpose heat source. In Proceedings of the 15th Intersociety Energy Conversion Engineering Conference, #809203, vol. 2, 1980, pp. 1032–1042.
2. Schock, A. and Or, C. T., Effect of fuel and design options on RTG performance versus PFF power demand. In Proceedings of the 29th Intersociety Energy Conversion Engineering Conference, vol. 1, 1994, pp. 535–540.
3. Schock, A., Or, C. T. and Kumar, V., Design modifications for increasing the BOM and EOM power output and reducing the size and mass of RTG for the Pluto mission. In Proceedings of the 29th Intersociety Energy Conversion Engineering Conference, vol. 1, 1994, pp. 541–547.
4. Schock, A., RSG options for Pluto fast flyby mission. 44th Congress of the International Astronautical Federation, Graz, Austria, IAF-93-R.I.425b, 1993.
5. Schock, A., Or, C. T. and Kumar, V., Radioisotope power system based on derivative of existing stirling engine. In Proceedings of the 30th Intersociety Energy Conversion Engineering Conference, #95159, vol. 1, 1995, pp. 649–656.
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