2009Unpublished venueRequires access

A method of CAE for calculating the temperature tolerance of telescope

Shaowang Xie, Zhu Xiaoming, Qingfen Li, Changzheng Chen

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Abstract

In order to obtain high quality pictures, the thermal design is necessary for the space telescope. The designed temperature scope should meet to the permissible temperature tolerance of the telescope. A method for calculating the permissible temperature tolerance of the telescope is studied. The calculating temperature tolerance will be targeted for space thermal environment adaptive structure design and thermal design. A method for describing the temperature fields of the telescope is introduced. The descriptive temperature fields are able to include every temperature states that the telescope endured on orbit. When the MTF (Modulation Transfer Function) just meet to the optical indicator, the ultimate temperature tolerance of the space telescope is obtained, that is, the aim temperature scope for the thermal design is obtained.

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What this paper is about

In order to obtain high quality pictures, the thermal design is necessary for the space telescope. The designed temperature scope should meet to the permissible temperature tolerance of the telescope. A method for calculating the permissible temperature tolerance of the telescope is studied. The calculating temperature tolerance will be targeted for space thermal environment adaptive structure design and thermal design. A method for describing the temperature fields of the telescope is introduced. The descriptive temperature fields are able to include every temperature states that the telescope endured on orbit. When the MTF (Modulation Transfer Function) just meet to the optical indicator, the ultimate temperature tolerance of the space telescope is obtained, that is, the aim temperature scope for the thermal design is obtained.

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Available abstract

In order to obtain high quality pictures, the thermal design is necessary for the space telescope. The designed temperature scope should meet to the permissible temperature tolerance of the telescope. A method for calculating the permissible temperature tolerance of the telescope is studied. The calculating temperature tolerance will be targeted for space thermal environment adaptive structure design and thermal design. A method for describing the temperature fields of the telescope is introduced. The descriptive temperature fields are able to include every temperature states that the telescope endured on orbit. When the MTF (Modulation Transfer Function) just meet to the optical indicator, the ultimate temperature tolerance of the space telescope is obtained, that is, the aim temperature scope for the thermal design is obtained.

Key concepts: Telescope, Spitzer Space Telescope, Scope (computer science), Thermal, Optical transfer function, Orbit (dynamics), Aerospace engineering, Optical telescope

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