EBAD
EBAD designs and manufactures non-explosive separation and release mechanisms for spacecraft, missiles, and launch vehicles. Its NEA® Payload Release Module (PRM™) carries high tensile preloads and releases with ultra-low shock below 500 g's, with flight heritage on multiple SpaceX Falcon 9 rideshare missions including Transporter 9, 12, and 15.
- Space Technology
- Defense Tech
- Hardware
- Aerospace
Funding
Founders
Founder details are not available yet.
Product
Problem
Spacecraft and missile systems require highly reliable separation and release mechanisms that function in extreme environments where failure is not an option. Traditional pyrotechnic devices generate high shock loads that can damage sensitive payloads, and non-explosive alternatives often lack the preload capacity, simultaneity, or flight heritage needed for critical missions.
Solution
EBAD provides a family of payload release modules (PRM™) and hold-down release mechanisms designed for satellite, missile, and launch vehicle applications. The NEA® PRM™ integrates a load-carrying interface, separation springs, and a bolt extractor into a turnkey dispensing mechanism that carries high tensile preloads until electrically commanded to release. Using a non-explosive spool-and-restraint-wire design with redundant fuse wires, the device provides ultra-low shock release with high simultaneity across multiple hold-down points. The PRM™ has been fully qualified for 4-point spacecraft dispensing applications and successfully deployed spacecraft on multiple SpaceX Falcon 9 rideshare missions, including Transporter 9, Transporter 12, and Transporter 15.
Target Audience
Primary customers are satellite manufacturers, launch vehicle integrators, and defense contractors who need qualified, flight-proven separation and release systems for spacecraft dispensing, stage separation, and missile payload deployment.
Features
- Ultra-low release shock below 500 g's (under 350 g's on PRM™ 9103A) for sensitive payload protection
- Redundant actuation circuit with firing times of 15 ms and release times under 20 ms at 6 amps
- Non-explosive hold-down and release function with no debris generation
- Configurable separation velocity and axial preload up to 8,500 lbf
- Can be operated with standard launch vehicle firing circuitry and includes a launch vehicle-to-payload connector interface
- Space-rated materials qualified to standard launch environments with factory refurbishment available
- NEA® hold-down release mechanism with more than 25 years of flight heritage and over 15,000 actuations
- Fully qualified for 4-point spacecraft dispensing per SpaceX Falcon 9 Rideshare Payload User's Guide (RPUG) standards