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Thermal Design, Test and Analysis of PharmaSat, a Small Class D Spacecraft with a Biological ExperimentSmall spacecraft have been increasing in popularity because of their low cost, short turnaround and relative efficiency. In the past, small spacecraft have been primarily used for technology demonstrations, but advances in technology have made the miniaturization of space science possible [1,2]. PharmaSat is a low cost, small three cube size spacecraft, with a biological experiment on board, built at NASA (National Aeronautics and Space Administration) Ames Research Center. The thermal design of small spacecraft presents challenges as their smaller surface areas translate into power and thermal constraints. The spacecraft is thermally designed to run colder in the Low Earth Orbit space environment, and heated to reach the temperatures required by the science payload. The limited power supply obtained from the solar panels on small surfaces creates a constraint in the power used to heat the payload to required temperatures. The pressurized payload is isolated with low thermally conductance paths from the large ambient temperature changes. The thermal design consists of different optical properties of section surfaces, Multi Layer Insulation (MLI), low thermal conductance materials, flexible heaters and thermal spreaders. The payload temperature is controlled with temperature sensors and flexible heaters. Finite Element Analysis (FEA) and testing were used to aid the thermal design of the spacecraft. Various tests were conducted to verify the thermal design. An infrared imager was used on the electronic boards to find large heat sources and eliminate any possible temperature runaways. The spacecraft was tested in a thermal vacuum chamber to optimize the thermal and power analysis and qualify the thermal design of the spacecraft for the mission.
Document ID
20090033819
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Diaz-Aguado, Millan F.
(NASA Ames Research Center Moffett Field, CA, United States)
VanOutryve, Cassandra
(San Jose State Univ. San Jose, CA, United States)
Ghassemiah, Shakib
(NASA Ames Research Center Moffett Field, CA, United States)
Beasley, Christopher
(Jacobs Engineering Group, Inc. Moffett Field, CA, United States)
Schooley, Aaron
(Jacobs Engineering Group, Inc. Moffett Field, CA, United States)
Date Acquired
August 24, 2013
Publication Date
March 7, 2009
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN-252
PK003
Distribution Limits
Public
Copyright
Other

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