Description
1.1 This specification covers the design and performance of unmanned aircraft system (UAS) launch system operating via a closed-loop pressurized hydraulic or pneumatic system with a hydraulic recovery, or both.
1.2 In instances where the launcher and UAS manufacturer are the same entity, compliance with this specification is the responsibility of the UAS manufacturer where applicable.
1.3 This standard does not purport to address all of the safety concerns associated with the USA launch system and its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.
Product Details
- Published:
- 08/01/2008
- Number of Pages:
- 7
- File Size:
- 1 file , 160 KB
- Redline File Size:
- 2 files , 320 KB
- Note:
- This product is unavailable in Russia, Ukraine, Belarus
