- Launch platform
- Air-launched from fighter-sized aircraft including A-4, A-6, and F-4 aircraft
- Guidance/control
- AQM-37A followed a pre-programmed flight path; later AQM-37C/D targets added command-control and reliability upgrades
- Propulsion
- North American/Rocketdyne LR64-NA-4 pre-packaged liquid-fuel rocket engine
- Speed
- Up to Mach 3 at high altitude; Cradle of Aviation exhibit lists 1,700 mph for its AQM-37A
- Altitude envelope
- About 1,000 ft to 80,000 ft for AQM-37A profiles, with later program use simulating ballistic profiles up to 300,000 ft
- Endurance
- About five minutes powered endurance after launch
- Weight
- 565 lb on the Cradle of Aviation AQM-37A exhibit
- Target features
- Pre-programmed flight path, radar-image projection, high-intensity flares, radar reflectors, and automatic destruct equipment are documented across museum and reference sources