Mechanical, Power, and Thermal Subsystem Design for a CubeSat
公开可下载的内容
open in viewerThe goals of this Major Qualifying Project (MQP) project were the design of thermal, mechanical, and power subsystems for a CubeSat supporting a university-led science mission to orbit an X-ray spectrophotometer. The spacecraft thermal analysis included calculation of unsteady temperature distributions over the course of several orbits. This analysis included radiation from the sun and earth as well as a preliminary analysis of heat generation from internal components. The mechanical design included component and assembly-level, solid models of several spacecraft configurations and a preliminary stress analysis. The power subsystem design included component selection for power generation, management, and distribution as well as energy storage.
- This report represents the work of one or more WPI undergraduate students submitted to the faculty as evidence of completion of a degree requirement. WPI routinely publishes these reports on its website without editorial or peer review.
- Creator
- Publisher
- Identifier
- E-project-031212-121649
- Advisor
- Year
- 2012
- Date created
- 2012-03-12
- Resource type
- Major
- Rights statement
关系
- 属于 Collection:
项目
单件
缩略图 | 标题 | 公开度 | Embargo Release Date | 行动 |
---|---|---|---|---|
Mechanical,_Power,_and_Thermal_Subsystem_Design_for_a_CubeSat.pdf | 公开 | 下载 |
Permanent link to this page: https://digital.wpi.edu/show/xp68kh975