Precision You Can Count On. Performance You Can Trust.

Designed to mount, hold, and release a spacecraft from the launch vehicle upper stage, or from another carrying spacecraft (OTV for instance).

Detects and validates proper sequencing of acceleration and separation environments and vehicle commanded inputs prior to activating internal arming inhibits.

Flight proven in Flight Termination Systems for many Tactical Missile and Launch Vehicles and have been qualified to extreme environments for FTS applications.

The EBAD NEA® HDRM is an electrically initiated, one-shot release mechanism that has the ability to carry a very high tensile preload until commanded to release.

A fully electronic, in-line device for rocket motor ignition. Housed by stainless steel, the ISD works by accepting DC electrical input power and arm/fire signals, performing safety logic validation, and generating high voltage for ignition of a Low Energy Exploding Foil Initiator (LEEFI) device.

A hermetically sealed stainless-steel body that houses the critical components of the device. The AFD contains dual electric detonators, and an electrically operated torque motor or rotary solenoid to rotate the detonators into the in-line (ARM) position.

Used for the ignition of solid rocket motors on strategic missiles, tactical missiles, and launch vehicles, and can be used in the initiation of hot gas generators.

EBAD manifolds connect energetic components with non-electric signal transfer systems. They ensure reliable transfer with controlled transfer interface geometry.