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STS 41-D Solar Array Flight Experiment

Gary F. Turner, Henry C. Hill

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Abstract

The Solar Array Flight Experiment (SAFE) developed under the direction of the Marshall Space Flight Center, scheduled for t launch on STS 41-D3 will demonstrate a lightweight solar array technology which offers a factor of 3 improvement in weight and a factor of 10 improvement in specific volume over solar array systems currently in use in the space program. The experiment^ which will include multiple deployment and retraction demonstration, verification of electrical and thermal performance* and verification of structural dynamic math models is 15 feet by 105 feet in size and^ if completely covered with solar cells.j would produce approximately 12.5 kW of electrical power. The unit has now been developed, tested, and is at Kennedy Space Center (KSC) being prepared for launch. This paper presents a summary of system design characteristics, ground test history, and present status.

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The Solar Array Flight Experiment (SAFE) developed under the direction of the Marshall Space Flight Center, scheduled for t launch on STS 41-D3 will demonstrate a lightweight solar array technology which offers a factor of 3 improvement in weight and a factor of 10 improvement in specific volume over solar array systems currently in use in the space program. The experiment^ which will include multiple deployment and retraction demonstration, verification of electrical and thermal performance* and verification of structural dynamic math models is 15 feet by 105 feet in size and^ if completely covered with solar cells.j would produce approximately 12.5 kW of electrical power. The unit has now been developed, tested, and is at Kennedy Space Center (KSC) being prepared for launch. This paper presents a summary of system design characteristics, ground test history, and present status.

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Available abstract

The Solar Array Flight Experiment (SAFE) developed under the direction of the Marshall Space Flight Center, scheduled for t launch on STS 41-D3 will demonstrate a lightweight solar array technology which offers a factor of 3 improvement in weight and a factor of 10 improvement in specific volume over solar array systems currently in use in the space program. The experiment^ which will include multiple deployment and retraction demonstration, verification of electrical and thermal performance* and verification of structural dynamic math models is 15 feet by 105 feet in size and^ if completely covered with solar cells.j would produce approximately 12.5 kW of electrical power. The unit has now been developed, tested, and is at Kennedy Space Center (KSC) being prepared for launch. This paper presents a summary of system design characteristics, ground test history, and present status.

Key concepts: Aerospace engineering, Software deployment, Photovoltaic system, Engineering, Electrical engineering, Software engineering

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