Title :
Pluto Express power system architecture
Author :
Carr, Gregory A.
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Abstract :
The Pluto Express power system must answer the challenge of the next generation spacecraft by reducing its power, mass and volume envelopes. Technology developed by the New Millennium Program will enable the power system to meet the stringent requirements for the Pluto Express mission without exceeding the spacecraft mass and volume budgets. Traditionally, there has been an increasing trend of the percentage of mass of the power system electronics with respect to the total spacecraft mass. With all of the previous technology focus on high density digital packaging, the power system electronics have not been keeping pace forcing the spacecraft to absorb a relative increase in the power system mass. The increasing trend can be reversed by using mixed signal ASICs and high density multi-chip-module (MCM) packaging techniques validated by the New Millennium Program. As the size of the spacecraft shrinks, the power system electronics must become tightly integrated with the spacecraft loads. The power system architecture needs the flexibility to accommodate the specific load requirements without sacrificing the capability for growth or reduction as the spacecraft requirements change throughout the development. Modularity is a key requirement that will reduce the overall power system cost. This paper describes how the combination of the New Millennium packaging technologies with the Pluto Express power system architecture will produce a product with the capability to meet a wide range of mission profiles while reducing system development costs
Keywords :
Pluto; hybrid integrated circuits; integrated circuit packaging; load (electric); mixed analogue-digital integrated circuits; power integrated circuits; power systems; space vehicle power plants; New Millennium Program; Pluto Express spacecraft; high density multi-chip-module packaging techniques; mission profiles; mixed signal ASICs; modularity; power system electronics; space power system; spacecraft mass; specific load requirements; Aerospace electronics; Costs; Electronics packaging; Integrated circuit packaging; Laboratories; Pluto; Power engineering and energy; Power systems; Space technology; Space vehicles;
Conference_Titel :
Energy Conversion Engineering Conference, 1996. IECEC 96., Proceedings of the 31st Intersociety
Conference_Location :
Washington, DC
Print_ISBN :
0-7803-3547-3
DOI :
10.1109/IECEC.1996.552843