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Space Fulcrum

Space Fulcrum designs and manufactures deployer mechanisms for CubeSat missions ranging from 1U to 16U, compatible with launch vehicles such as Falcon 9 and PSLV. Their product line includes the TA HDRM torque motor (1–20 mNm) and the TA RW release system, both built with lightweight aluminum housings and dual‑redundant actuation for high reliability.

Vojka, VojvodinaFounded 20232200+ followers
Updated 1 month ago

Funding

Funding not disclosed

Funding rounds are not available yet.

Founders

Founder details are not available yet.

Product

Problem

CubeSat missions require compact, reliable deployment mechanisms that can fit a range of satellite sizes and meet strict launch vehicle and NASA environmental standards. Inadequate deployers can lead to deployment failure, mission loss, or costly redesigns to satisfy launch provider requirements.

Solution

Space Fulcrum provides purpose‑built deployer mechanisms for CubeSats ranging from 1U to 16U, engineered for compatibility with launch vehicles such as Falcon 9 and PSLV. Their product line includes the TA HDRM torque motor, offering selectable torque from 1 mNm to 20 mNm, and the TA RW release system, featuring a dual‑redundant actuation design for high reliability. Both devices use lightweight aluminum housings with integrated thermal paths to minimize mass while maintaining structural integrity. The company also offers advanced testing services that verify compliance with NASA GAVS environmental verification standards, ensuring that each deployer meets the performance and durability criteria required for launch.

Target Audience

Primary customers are CubeSat manufacturers and mission integrators that need certified deployment hardware for satellites up to 16U, as well as launch service providers requiring compliant payload interfaces.

Features

  • TA HDRM torque motor available in three sizes for 3U, 6U, and 12U buses, delivering 1–20 mNm torque
  • TA RW release mechanism with dual‑redundant actuation for secure attachment and reliable release
  • Lightweight aluminum housing with integrated thermal path for efficient heat dissipation
  • Compatibility with major launch vehicles (Falcon 9, PSLV) and adherence to NASA GAVS standards
  • Simple electrical interface for straightforward integration with satellite onboard systems
  • Advanced testing services, including environmental verification and thermal analysis, to certify deployer performance
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