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Deployable Lunar Hopper (Hopper-TP)

Completed TRL 5 (started at 5, targeting 7)

Description

The lunar deployable hopper project (Hopper) started as a Tipping Point proposal, submitted by Intuitive Machines (IM) in July of 2020. The project was kicked off in March of 2021. The project successfully developed, assembled, tested and operated a small robotic hopper. This deployable lunar hopper (µ-Nova "Grace") flew to the lunar surface in early 2025 on a Nova-C lander through a commercial mission (IM-2), leveraging mature landing system technologies developed for the Nova-C platform by Intuitive Machines. Due to the off-nominal landing orientation, the Hopper surface operations were constrained and it did not deploy from the lander. Hopper is intended to be deployed as a secondary payload from a NASA Commercial Lunar Payload Services (CLPS) lander, providing access to extreme environments and locations of interest on the lunar surface. At the cost of a secondary payload on a small CLPS lander, Hopper enables lunar surface science and human exploration by providing targeted access for different types of payloads and mission profiles to extreme locations on the lunar surface.  Among its technical capabilities, Hopper can operate in a Permanently Shadowed Region (PSR) for a limited duration, autonomously fly into and out of PSRs, carry up to a 10 kg payload (range dependent), and “hop" the payload up to 25 km (ballistic transfer with current tank configuration).  Communications with Hopper utilize the lander or orbital assets as a relay station.  The Hopper records payload data to its on-board computer and transmits the data once line-of-sight to the lander is restored.  The Hopper design is also scalable to larger payloads and travel range.

Benefits

A deployable robotic hopper (𝜇-Nova) will provide access to extreme locations and environments not accessible by humans in EVA suits, rovers, or other technologies. 𝜇-Nova is enabling for lunar surface science by providing a low-cost secondary payload option for Commercial Lunar Payload Services (CLPS) landers. The platform is flexible to accommodate different payloads on different mission profiles.  The hopper will be able to operate in a permanently shadowed region (PSR) and will autonomously fly into and out of the PSR.  Other mission types enabled by the proposed technology include access into lunar pits with vertical sidewalls and regional prospecting of multiple dispersed surface sites. Because of the way it travels, μ-Nova can quickly traverse between sites of interest, leaving more time for principal investigators to process data and to make decisions about the mission.  This hopper significantly increases science return and lunar terrain accessibility. Through this Tipping Point demonstration, subsequent mission costs, system complexity and mass will be reduced. Additionally, the risk to future similar missions is reduced.​

Details

Technology areaRobotic Systems > Mobility > Above-Surface Mobility
ProgramGame Changing Development (GCD)
Lead organizationJohnson Space Center, Houston, TX
Start date2021-03-01
End date2025-05-31

Project contacts

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