MGX Minerals Announces Driftwood Creek Magnesium Specification Parameters for Mg Solid Rocket Fuel for Mg/CO2 Type Rockets
Mg/CO2 Rockets for Mars Ascent
By reducing the traditional propellant requirement for ascent from Mars the engine size and mass of spacecraft may be reduced. With an atmosphere of 97% carbon dioxide, CO2 is readily available on Mars. Magnesium is one of the lightest known metal solid propellants.
Magnesium Solid Rocket Fuel Design Parameters
In a Mg/CO2 propulsion system, the magnesium powder may be fed by a positive displacement fluidized bed feed system, which includes a porous piston in a cylindrical tank. The piston pushes the powder, and the gas fluidizes the powder at the same time. Particle size distribution, particle shape, and the purity of the magnesium have been determined as the primary parameters. The Company is focused on a high purity magnesium particle with a small particle size of <50 micron. The smaller the particles, the shorter the burning time, which is desirable for complete burning of the fuel inside the combustion chamber. A priority is to reduce the size of the fuel storage tank by using a higher density material. The characteristics of the feeding process are sensitive to the powder characteristics, such as the particle size distribution and the shape of the particles. In the feeding process, a lower density particle may be a positive factor. This will require a balanced final particle optimization that considers a preference for high density magnesium particles balanced with a potential decrease in the feeding flow rate or creation of significant variation in pressure, deposition in the pre-burner, and overall efficiency. Both regular and irregular shaped particles are being considered at this time.
Mg/CO2 Type Rocket Engines
The ignition, combustion, and performance of magnesium carbon-dioxide type rocket engines have been experimentally studied. The ignition temperature of magnesium particles of medium sizes in CO2 is about 960 K. Although broad applications may exist for powder fuel rockets, Mg/CO2 engines have been primarily studied for Mars exploration, ascent and return to Earth by NASA, due to the abundance of CO2 on Mars.
Recent experimental studies have been carried out on the characteristics of powdered Mg feed, CO2 liquid feed, engine ignition, combustion, and pressure oscillation. Results show stability in the feeding systems with stable feed and performance characteristics. The Damköhler number, L/[vj?×?(ti + tb)], incorporates the parameters of pre-combustion chamber length, powder-injection velocity, particle ignition delay, and burning time. Successful ignition is indicated by Damköhler number >1. Reliable ignition and a stable flame has been achieved.
Driftwood Creek Magnesium Project
MGX has completed a Preliminary Economic Assessment ("PEA") for the Driftwood Creek magnesium project (Tuun, 2018). The PEA references report title "Driftwood Magnesite Project Mineral Resource Estimate, Brisco, BC", author Allan Reeves, P.Geo, report date September 30, 2016, revised July 21, 2017. The resource highlights are listed as follows:
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- Measured 2.8 million tonnes grading 43.3%plus Indicated 5.2 million tonnes grading 43.3% (M+I) mineral resource totaling 8.028 million tonnes grading 43.3% magnesium oxide (MgO)
- Inferred mineral resource totaling 846,000 tonnes grading 43.20% MgO
- Bulk of resource is located less than 100 meters from surface
Qualified Person
Andris Kikauka (P. Geo.), Chief Executive Officer of MGX Minerals, has prepared, reviewed and approved the scientific and technical information in this press release. Mr. Kikauka is a non-independent Qualified Person within the meaning of NI 43-101.
About MGX Minerals Inc.
MGX Minerals is a diversified Canadian resource and technology company with interests in advanced metals, industrial minerals, and energy technologies.
Contact Information:
Andris Kikuaka
Chief Executive Officer
andris@mgxminerals.com
604 681 7735
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