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LUNAR OXYGEN TECHNOLOGIES

We work with everyone:​

  • Lunar Lander Manufacturers

  • Satellite and Spacecraft Manufacturers

  • Aerospace Component Manufacturers

  • Custom Metal Fabricators

  • General Purpose Manufacturers

  • Importers/Exporters

  • Businesses in Flexible Packaging

  • Academic Institutions

  • Government Institutions

  • Businesses in Flexible Packaging

  • Businesses in Industrial Glass Processing

  • Businesses in Food Services and Processing

What we can help with:​

  • ISRU System Design and Development

  • Requirements and Constraints Development

  • Space Systems Engineering

  • Supply Chain Management

  • Sales and Business Development

  • General Product Development

  • Rapid Prototyping

  • Design for Manufacturing

  • Machining/Welding/Fabricating

  • CAD & FEA (Structural & Thermal)

  • Design of Experiments

  • Technical Proposals

ISRU PRODUCTS

Lunar Oxygen.jpg

Lunar Oxygen is a horizontally scalable two-stage modular system that can extract volatile gases and oxygen from lunar regolith. The hollow ionizing cathode, slide contact surfaces, and the tumbling heated reactor enable this system to be compact and user-friendly.

AEROSPACE PRODUCTS

RALS_2016_edited.jpg

Reduced Altitude Launch System (RALS) V2 is a state-of-the-art platform that can be used to launch payloads from a height ranging between 10 kilometers to 40 kilometers. This system relies on a robust supply chain that can allow for 10,000+ units to be manufactured and deployed at a moments notice.

MEET THE TEAM FOR RALS V2

Monty Sasnauskas

System Operations Lead Engineer

Responsible for leading all innovative modifications, team meetings, system integration efforts, subsystem mass tracking, launch protocols, recovery of RALS, and gas loading configuration.

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Albert Barcelon

Avionics Lead Engineer

Responsible for leading the avionics subsystem design, programming actuators and sensors, component characterizations, soldering, and wiring.

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Riley Bertaux

Structures Lead Engineer

Responsible for leading the arm and central structure design, material selection of structure, developing all CAD parts and assemblies, FEA analysis of the structure, and the budget.

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Samuel Schroeder

Rocket Lead Engineer

Responsible for leading all rocket preparations, recovery of the rocket, rocket ignition, rocket structure subsystem, and propulsion subsystem.

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Noah Cisneros

Manufacturing Lead Engineer

Responsible for leading the coordination of all manufacturing efforts (FDM, Routers, Mills, Saws), managing the manufacturing schedule, transportation of all systems, and ordering all materials including PPE.

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Randy Olguin

Test Lead Engineer

Responsible for leading the coordination of all testing efforts (leak tests, beam bending tests, balloon lift tests), overseeing all FAR (Friends of Amateur Rocketry) relations, and programming all testing data acquisition systems.

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