Thermal Design of the Lunar Exploring Spacecraft Institute of Space and Astronautical Science

Format:

Conference/Event

Author/Creator:

Ohnishi, A. (Akira), author.

Conference Name:

International Conference on Environmental Systems (1997-07-14 : Lake Tahoe, Nevada, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1997

Summary:

The thermal design of the LUNAR-A spacecraft, investigating the internal structure of the moon, is a challenge due to the widely varying thermal environments. A passive thermal control philosophy of radiators, multilayer insulation (MLI) and heaters was used for the LUNAR-A thermal design. Verification of the design was performed separately for the major spacecraft modules which consisted of a main structure, a propulsion subsystem and penetrators. As consequence, acceptable thermal performance can be expected for all phases of the mission. This paper describes the thermal design, analysis, thermal model testing and in-orbit temperature predictions

Notes:

Vendor supplied data

Publisher Number:

972469

Access Restriction:

Restricted for use by site license