Rocket Plume Excavation for Deep Frozen Volatile Mining

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Solution Overview

Problem

Current methods for mining frozen volatiles in space, such as lunar ice, are inefficient due to high mechanical complexity, depth limitations, and maintenance requirements, and lack the ability to effectively excavate deep deposits and process resources quickly and economically.

Innovation Solution

The use of a rocket engine plume to create a controlled pressure environment, generating a deep cratering effect through standing shock waves, which allows for efficient excavation and processing of frozen volatiles by heating and releasing them from the regolith, and subsequent condensation using a collection manifold and cold trap system.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If traditional drilling methods are used to mine frozen volatiles, then mechanical complexity and maintenance requirements increase, but excavation depth and efficiency are limited

Engineering Contradiction:
Improvemining efficiencyVSAvoidmechanical complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The patent replaces traditional mechanical drilling systems with a rocket engine plume-based thermal excavation system. The rocket plume uses thermal energy and shock waves to melt and excavate frozen volatiles, eliminating complex mechanical drilling components and reducing maintenance requirements while increasing mining depth and efficiency

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The system changes the operating parameters by using controlled pressure environments and varying rocket engine thrust levels to create different plume characteristics. This allows the same system to adapt to different mining depths and volatile concentrations without mechanical reconfiguration

Inventive Principle:
Principle #35Parameter changes

2Length of stationary object

If traditional drilling methods are used, then the system can operate with simple equipment, but it cannot effectively excavate deep deposits

Engineering Contradiction:
Improveexcavation depthVSAvoidresource extraction rate
Core Design Contradiction:
Length of stationary objectVSProductivity

Solution Approach 1:

The rocket engine can operate continuously or in repeated pulses to progressively deepen the excavation crater, allowing sustained access to deep volatile deposits. The system maintains continuous thermal action on the regolith, preventing the need to retract and reposition equipment as depth increases

Inventive Principle:
Principle #20Continuity of useful action

3Length of stationary object

If the rocket engine is positioned closer to the ground to increase excavation depth, then the plume energy is more concentrated, but the collection manifold must handle higher pressures

Engineering Contradiction:
Improvecrater depthVSAvoidcollection manifold pressure
Core Design Contradiction:
Length of stationary objectVSStress or pressure

Solution Approach 1:

The system dynamically adjusts the rocket engine thrust level and pulse duration based on real-time pressure sensors in the collection manifold. When the manifold approaches maximum pressure capacity, the system reduces thrust or extends pulse intervals, allowing the engine to be positioned close to the ground for deep excavation while maintaining safe operating pressures

Inventive Principle:
Principle #15Dynamics

4Area of stationary object

If the plume is allowed to expand freely, then the excavation area is larger, but the energy concentration at the target decreases

Engineering Contradiction:
Improveexcavation areaVSAvoidplume temperature at target
Core Design Contradiction:
Area of stationary objectVSTemperature

Solution Approach 1:

The rocket engine operates in periodic pulses rather than continuous flow. Each pulse creates a concentrated plume that penetrates to the target depth, then pauses to allow volatiles to be collected and pressure to equalize. This periodic action maintains high temperature concentration while achieving sufficient excavation area through repeated passes

Inventive Principle:
Principle #19Periodic action

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This method enables efficient and cost-effective mining of deep deposits of frozen volatiles, reducing mechanical complexity and maintenance needs, while allowing for the extraction of resources beyond the reach of traditional drilling methods, with the potential for continuous operation and sustainable resource extraction.

Implementation Method 1

aiming the plume into or through the ground to heat a frozen volatile source within the ground or underground

Methodology Applied
Scientific EffectThermal conduction: Conduction (thermal)

Implementation Method 2

combusting propellant within a rocket engine and creating a plume

Methodology Applied
Scientific EffectConvection: Convection

Implementation Method 3

cold processing the volatiles in a condenser to condense the volatiles into liquid or solid form

Methodology Applied
Scientific EffectCondensation: Condensation

Implementation Method 4

generating a deep cratering effect through standing shock waves

Methodology Applied
Scientific EffectShock wave: Shock Wave

Data Source

PatentUS11852016B2Rocket mining system, subsystems, components and methods
Publication Date: 2023.12.26 ASTROBOTIC TECHNOLOGY INC
  • US11852016B2 patent drawing
  • US11852016B2 patent drawing
  • US11852016B2 patent drawing

AI summary

Mining apparatuses, systems and methods related to the use of a rocket engine's plume and a collection manifold to efficiently displace, collect, process and store frozen volatiles embedded within or below a surface is disclosed. The plume contacts and churns up the surface. The frozen volatiles are displaced and/or evaporated within a closed environment under a collection manifold. The collection manifold has related components for addressing these frozen or gaseous volatiles downstream. Various apparatuses and subsystems are also disclosed including a rover, processing plants, collection manifold, and vapor manifold.