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SPACE ACT UMBRELLA AGREEMENT NO. SAA8-1930516 ANNEX NO. SAA8-1930516.2
May 19th, 2020
  • Filed
    May 19th, 2020

This Annex shall be for the purpose of providing unique NASA/MSFC expertise for modeling propellant and pressure feed system dynamic transients for the Astrobotic's Peregrine robotic cargo lunar lander propulsion feed system by adapting the Easy5 Advanced Controls & Systems Simulation computer software tool. The initial design and development of the Astrobotic Peregrine lunar lander was started under the now completed NASA Lunar Cargo Transportation and Landing by Soft Touchdown (Lunar CATALYST) initiative. This reimbursable Annex is the next logical step under currently active Commercial Lunar Payload Services (CLPS) initiative to support the continued progress of the propulsion design though analytical design and system testing.

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