TESTING CAPABILITIES
AVET Lab Abilities
- Adhere to standard test method as outlined by F3389/F3389M
- Able to meet all impact orientations as outlined by F3389/F3389M 鈥� Method B, C, & D
- Able to accommodate most small unmanned aircrafts (sUA) Categories 1, 2, & 3
- Capable of achieving both critical speeds & operational speeds for most sUAs
- Adaptability of test apparatus allows for fixed-wing & rotor-wing sUAs, sUA parts, and rigid impactors
- Worst case testing for probable impact orientations
- Photographic & video documentation of testing procedures
- Data collection using data aquisition, instrumentation, and photometric analysis per SAE J211
- Generation of reports with data analysis & results
sUA Impact Launcher with Rigid Seat
- Adjustability to allow for vertical drops, horizontal impacts, and angled impacts
- Ability to adjust launch speeds to meet various velocity requirements
- Attachable sled permits a variety of fixtures to be mounted to accommodate the variation in sUA orientations
- Lift table with fixed mounting plate provides adjustability and stability
- Rigid Seat offers ability to restrain FAA HIII ATD to increase stability and repeatability
of impacts
