Lunar Tether–Delivered Rover Swarms for Sun-Synchronous Traversal

This page outlines a proposed sequence of space tether development missions, beginning with lowering small payloads to the Moon and culminating in distributed, fault-tolerant rover swarms capable of near-continuous sunlight traversal.

The core idea is to trade single large rovers for cooperating swarms of small, tether-delivered robotic payloads that can physically link together, share power and functions, and tolerate multiple failures without total mission loss.

1. Mission Motivation

Continuous or near-continuous access to sunlight on the Moon dramatically simplifies power, thermal management, and operations. However, the surface speed required to remain in sunlight depends strongly on latitude:

Latitude Required Average Speed Approx. Earth Speed
0° (Equator) 4.67 m/s ≈ 10.5 mph
85° 0.37 m/s ≈ 0.8 mph

Achieving equatorial sun-synchronous traversal with a single small rover is extremely challenging. Achieving it with a cooperative train of rovers may be feasible.

2. Tether-Delivered Architecture

A rotating lunar orbital tether is assumed, capable of lowering payloads gently to the surface. Key features:

The tether does not need to deliver a single large rover. Instead, it delivers a self-assembling surface system.

This approach lowers per-payload cost, reduces risk, and allows partial mission success even with individual failures.

3. Rover Swarm / Train Concept

Ten 10-kg rovers form a physically connected “train” or swarm. Each rover is a peer, not a disposable unit.

Key Principles

The result is a distributed, fault-tolerant solar-electric locomotive operating on the lunar surface.

4. Mechanical Coupling and Locomotion

Rovers connect via a simple, robust mechanical coupling:

This design reduces mass, software complexity, and power consumption for non-lead rovers.

Rolling Resistance Advantage

Following rovers roll on compacted regolith created by the lead rover, reducing rolling resistance and required traction. By rotating which rover leads, wear and power demand are shared across the swarm.

5. Power Sharing and Energy Management

Each rover carries its own solar panels and power electronics. When connected:

At equatorial speeds (~10.5 mph), plowing would be used only sparingly, primarily to escape difficult terrain rather than for continuous operation.

6. Assembly on the Surface

The swarm assembles incrementally:

  1. Rover 1 lands and begins moving along the equator.
  2. Rover 2 lands ~2 hours later nearby; Rover 1 rendezvous and couples.
  3. Rovers 1–2 move together to meet Rover 3.
  4. The process repeats until the full train is assembled.

This bootstrapping approach avoids the need for precision landing of all payloads in a single spot.

7. University-Based Competitive Mission Model

A proposed program structure:

Design Freedom

Universities may allocate mass however they wish:

This creates a real, flight-ready robotics competition rather than a purely academic exercise.

8. Technical Evaluation

Strengths

Challenges

Mitigations

9. Overall Assessment

Trains or swarms of ten 10-kg rovers appear plausible as an early lunar surface system enabled by tether delivery. The concept leverages redundancy, incremental assembly, and competition to tackle one of the hardest problems in lunar exploration: high-speed, long-duration, solar-powered traversal.

Even if equatorial sun-synchronous travel proves too ambitious initially, the architecture remains valuable for polar and mid-latitude missions—and provides a natural evolutionary path toward larger, more capable lunar infrastructure.