SBIR/STTR Research Award

Lithium-Ion Battery Solid Rocket Motor for Deorbit Applications

Award identifier afd95b32a34c399de7bfd92ba7accc83226ee2640c9681dc4c424a5de8e98029Awarding agency National Aeronautics and Space Administration

Award amount

$159,696

Program and phase

SBIR · Phase I

Award year

2023

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
CAIRN ENGINEERING LLC
Proposal award date
2023-07-31
Contract end date
2024-02-02
UEI
VRTRZ5EQPJW6
Solicitation number
SBIR_23_P1
Topic code
Z8

Research abstract

Our proposed innovation is the Lithium-Ion Thruster (LIT) system, a multi-use device capable of both electrical energy storage and thrust generation using the same hardware. The LIT system is an ideal candidate for a NASA Phase I SBIR grant because proving its feasibility will introduce a new propulsion and battery technology that provides distinct advantages over all other deorbiting technologies. It will do this by creating a massless battery within the propulsion system, using the stored energy inside the battery to power the spacecraft during normal operations, and then converting that same energy into thrust when the mission is complete. This unique coupling of systems reduces the overall size, weight, and power draw of the propulsion and battery system while also increasing the energy storage available. This allows spacecraft designers to dedicate more resources to the payloads they need to accomplish their science, commercial, and defense objectives while including a system to effectively deorbit spacecraft to reduce crowding and collision risk in low Earth orbit (LEO).This novel technology improves on traditional propulsion systems in the following ways: ● Combining the battery and propulsion system into a single device creates massless hardware by using the same mass for two distinct purposes. Volume, power draw, and cost will also be reduced, allowing more resources to be dedicated to the spacecraft payloads. ● Electrical energy storage capacity of the spacecraft will be increased, reducing pressure on mission designers with tight power budgets. ● The thrust of a burn can be controlled by altering the charge state of the battery cell. ● System safety will be increased during high-risk activities, such as handling, transportation, or launch, by putting the batteries into a low energy state (effectively unfueling the system). The battery cells can then be charged to the appropriate level on orbit before a propulsive event.

Technology keywords

Not reported

Agency intelligence

National Aeronautics and Space Administration

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