Modular, Reconfigurable, High-Energy Systems Stepping Stones

Paper number

IAC-05-D3.2.04

Author

Mr. Joe T. Howell, National Aeronautics and Space Administration (NASA), United States

Coauthor

Mrs. Connie K. Carrington, National Aeronautics and Space Administration (NASA), United States

Coauthor

Mr. John C. Mankins, ARTEMIS Innovation Management Solutions, LLC, United States

Year

2005

Abstract

Modular, Reconfigurable, High-Energy Systems are Stepping Stones to provide capabilities for energy-rich infrastructure strategically located in space to support a variety of exploration scenarios.  Abundant renewable energy at lunar or L1 locations could support propellant production and storage in refueling scenarios that enable affordable exploration. Renewable energy platforms in geosynchronous Earth orbits can collect and transmit power to satellites, or to Earth-surface locations.  Energy-rich space technologies also enable the use of electric-powered propulsion systems that could efficiently deliver cargo and exploration facilities to remote locations.

A first step to an energy-rich space infrastructure is a 100-kWe class solar-powered platform in Earth orbit. The platform would utilize advanced technologies in solar power collection and generation, power management and distribution, thermal management, and electric propulsion. It would also provide a power-rich free-flying platform to demonstrate in space a portfolio of technology flight experiments.

This paper presents a preliminary design concept for a 100-kWe solar-powered satellite with the capability to flight-demonstrate a variety of payload experiments and to utilize electric propulsion.  State-of-the-art solar concentrators, highly efficient multi-junction solar cells, integrated thermal management on the arrays, and innovative deployable structure design and packaging make the 100-kW satellite feasible for launch on one existing launch vehicle. Higher voltage arrays and power management and distribution (PMAD) systems reduce or eliminate the need for massive power converters, and could enable direct-drive of high-voltage solar electric thrusters.

Abstract document

IAC-05-D3.2.04.pdf

Manuscript document

IAC-05-D3.2.04.pdf (🔒 authorized access only).

To get the manuscript, please contact IAF Secretariat.