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Latest Developments in Canadian Lunar Rover Prototypes

机译:加拿大农场型原型的最新发展

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In late 2014, Ontario Drive and Gear Ltd. (ODG) and its partners, including Canadensys Aerospace Corporation, commenced development of two new lunar/planetary rover prototypes for the Canadian Space Agency (CSA): the Lunar Rover Platform and Drivetrain Prototype (LRPDP) and the Small Planetary Rover Platform (SPRP). Both of these rovers build on ODG's significant heritage from several previous generations of lunar rover prototypes, including Juno and Artemis Jr., which were used by CSA and NASA in multiple analogue deployments starting in 2010. Completed in the first half of 2016, these two new rovers demonstrate the compatibility of the ODG rover architecture with higher Technology Readiness Levels (TRLs), including a TRL-6 drivetrain, as well as next-generation semi-compliant metallic wheels that are designed to remain compliant over a wide thermal range. LRPDP is a mid-size mobility platform characterized by a robust, simple architecture that places an emphasis on functionality in extreme terrain such as soft regolith, steep slopes, and rocky surfaces. All sensitive components such as motors, gearboxes, and avionics are located in sealed compartments for thermal control and dust contamination protection. The chassis design accommodates a large payload in the center of the rover footprint. The rover mass is 112 kg with an allowable payload of up to 160 kg. SPRP is similar to LRPDP, but is optimized for smaller size. It features a unique chassis designed to provide both thermal and contaminant protection for the avionics and power systems while providing quick access to payloads during testing. It also includes a reconfigurable suspension. The vehicle mass is 94 kg with an allowable payload of 50 kg. TRL-6 thermal vacuum testing of a drivetrain assembly was conducted at NASA Glenn Research Center (GRC) in Cleveland, Ohio in late 2015. The VF13 vacuum chamber used at GRC allowed the equipment to be tested with lunar simulant present under exposure to thermal extremes. The drivetrain assembly performed as designed during the test. Analog performance testing was also conducted on both LRPDP and SPRP, equipped with next-generation semi-compliant metallic wheels. The rovers performed as designed. The successful completion of testing on the LRPDP and SPRP rovers showed that this latest generation of Canadian lunar rover prototypes provides highly-capable and cost-effective platforms that represent the next step in the development of a fully flight-qualified Canadian lunar rover for a future mission.
机译:2014年底,安大略省驱动器和齿轮有限公司(ODG)及其合作伙伴,包括Canadensysy Aerospace Corporation,开始开发加拿大航天局(CSA)的两个新的月球/行星流动癖原型(CSA):​​Lunar Rover平台和动力传动系统原型(LRPDP )和小行星流动站平台(SPRP)。这两个人都对ODG的重要遗产来自几代几代农场原型,包括朱诺和Artemis Jr.,CSA和NASA在2010年开始的多个模拟部署中使用。2016年上半年完成,这两个新的Rovers展示了ODG Rover架构具有更高技术准备水平(TRL)的兼容性,包括TRL-6动力传动系统,以及设计用于保持符合宽热范围的下一代半兼容金属轮。 LRPDP是一个中型移动平台,其特征是由强大的简单架构,可强调极端地形中的功能,如柔软的石油,陡坡和岩石表面。所有敏感元件,如电机,齿轮箱和航空电子设备都位于密封隔室中,用于热控制和粉尘污染保护。底盘设计在流动站占地面积中有一个大的有效载荷。流动站质量为112千克,允许有效载荷高达160公斤。 SPRP类似于LRPDP,但针对较小尺寸进行了优化。它具有独特的底盘,旨在为航空电子和电力系统提供热和污染物保护,同时在测试期间快速访问有效载荷。它还包括可重构的悬浮液。车辆质量为94千克,允许有效载荷为50千克。在2015年底,在俄亥俄州克利夫兰的NASA Glenn研究中心(GRC)在NASA Glenn研究中心(GRC)进行了TRL-6热真空测试。GRC中使用的VF13真空室允许通过暴露于热极端的月球模拟剂测试设备进行测试。驱动器组件如测试期间设计。还在LRPDP和SPRP上进行模拟性能测试,配备了下一代半符合金属轮。这些流浪者如同设计。成功完成对LRPDP和SPRP ROVER的测试表明,这一最新一代的加拿大月球流动架原型提供了高度的能力和成本效益的平台,该平台代表了开发完全飞行合格的加拿大月球流动站的下一步使命。

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