MIL MIL-DTL-27422F PDF

This specification covers the requirements and verification testing for crash-resistant, ballistic-tolerant fuel cells for use in fixed wing and rotary-wing aircraft (including tilt rotor). Exact design criteria such as fuel cell dimensions, total weight, and interface requirements will be dependent upon the intended aircraft specified in the contract or purchase order.

File Size :	1 file , 3.1 MB
Note :	This product is unavailable in Ukraine, Russia, Belarus
Number of Pages :	45
Published :	02/06/2014