Black and white drawing of a person setting a fire in a small pile of logs in a fire pit amidst decorated autumn leaves, pumpkins, and a pumpkin-shaped container.
A spacecraft with gold foil insulation and solar panels on the moon's surface, featuring multiple wheels for mobility and a tall antenna or instrument on top.

The H.A.R.V.E.S.T. Rover (Habitat Assessment, Resource Validation, and Exploration System Technology) is a Lunar Cave Exploration Mission designed as a precursor for human habitation on the Moon. The rover will assess the habitability and resource potential of the Lacus Mortis Pit, a lunar cave with stable temperatures and a natural entrance ramp.

Its two primary objectives are:
1. Developing robotic exploration capabilities for future lunar missions.
2. Evaluating habitation systems by assessing safety, infrastructure needs, and structural integrity.

Technical engineering drawing of a tracked vehicle with multiple views: top, side, front, and isometric, including measurements and labeled parts.

Driving Requirements and Constraints:

The mission operates under strict engineering and logistical constraints, including:
- Mass Limit: The rover must not exceed 350 kg.
- Dimensions: The maximum allowable size is 2.0m × 1.25m × 1.25m.
- Budget: The mission is capped at $300M.
- Timeline: The rover must be launch-ready by March 1, 2030.

While the mass, dimensions, and timeline constraints are met, cost reductions or additional funding will be required to stay within budget.

A robotic or mechanical device with wheels and joints navigating a sloped surface.



The H.A.R.V.E.S.T. Rover is built on a rocker-bogie suspension system, which enables efficient traversal of rough lunar terrain.
Key specifications:
- Height: 0.986m
- Length: 1.971m
- Width: 1.250m
- Mass: 350 kg
- Power Consumption: 2,520 W

The design prioritizes mobility, durability, and adaptability for extended exploration and data collection in extreme lunar conditions.

Vehicle Design Overview

A robot with four black wheels and a metallic body, positioned in a studio with lighting equipment in the background.



Mechanical System: Inspired by the Curiosity Rover, the wheel design mitigates regolith accumulation and withstands temperature fluctuations.

Power System: Solar panels and battery storage ensure continuous operation. Batteries are shielded from temperature variations to prevent degradation.

Thermal System: Passive and active heat management prevents overheating and cold-soaking of critical components.

Computing and Data Handling (CDH): The system is radiation-shielded to prevent data corruption and ensures reliable storage and transmission of mission data.

Mechanical and Power Systems

A lunar surface map showing craters, with a red highlighted crater and a white crater, on a computer screen with various mapping and analysis tools.



H.A.R.V.E.S.T. is equipped with advanced instruments to study the lunar surface and subsurface:
- ChemCam (LIBS): Determines regolith composition via Laser-Induced Breakdown Spectroscopy.
- CheMin: Analyzes mineral content for resource utilization.
- RIMFAX (GPR): Ground-penetrating radar for subsurface geological mapping.
- LiDAR: Generates 3D terrain maps of the lunar pit interior.
- Thermal Imager: Monitors surface and subsurface temperature fluctuations.
- Radiation Monitor: Assesses habitability by measuring radiation exposure.
- Seismometer: Evaluates structural stability and profiles lunar seismic activity.

These instruments will provide critical data for future lunar missions, aiding in site selection for potential human settlements.

Science Instrumentation and Payload