原文传递
Mars sample return power supply
| 题名： | Mars sample return power supply |
| 作者： | Hoang, Don; Ludwigs, Sharon; Schmitz, Paul; Wright, John |
| 关键词： | sample；supply；retur；mars；turn；power；redundancy；collection；reliability；components |
| 摘要： | A power supply is designed for a vehicle able to operate on the surface of Mars for a period of 5 to 10 years. This vehicle will be used for sample and data collection. The design is based on the assumption that the vehicle will be unmanned. Also, there will be no means by which components could be repaired or replaced while on the Martian surface. A consequence of this is that all equipment must meet high standards of reliability and, if possible, redundancy. Power will be supplied to the vehicle by means of a General Purpose Heat Source capable of producing a minimum of 7 kW of thermal power. The heat generated from the General Purpose Heat Source will be transferred to a Stirling engine via hot side heat pipes. The Stirling engine will then convert this heat into 2 kW of electrical power. Cold side heat pipes will be used to carry away waste heat, which will be released to the Martian environment via radiators connected to the end of the cold side heat pipes. |
| 报告类型： | 科技报告 |
相关文献
- Different Classes of TPS Architectures and the Influence of Material and Architecture on Failure Mode Evolution and Mars Sample Return: Grand Challenge for EDL.
- Mobile Aircrew Restraint System - MARS
- Development Concepts for Mars Ascent Vehicle (MAV) Solid and Hybrid Vehicle Systems.
- Mobile Aircrew Restraint System - MARS. Conference paper.
- Conducted Electrical Emissions from Type L-858 Style 2 and 3 Airfield Signs. Technical note.
- Pterodactyl: Development and Evaluation of Control Designs for a Mechanically Deployed Entry Vehicle.
检索历史
应用推荐
