Detailed Specification Sheet: Nozzle, Probe, Aerial Refueling, Type MA-2

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Abstract:

REQUIREMENTS: 1. Where specified, surface roughness 63/, ASME-B46.1. 2. Remove all burrs and break sharp edges .010 to .020. 3. Dimensions in inches. Unless otherwise specified, tolerances: Decimals + or - .010, Angles + or - 1/2 degree. 4. At assembly where nozzle is threaded into the probe mast nose, MS24359, lock securely in place with the lock ring, MS24360-2, 1 required. 5. For use with reception couplings designed and qualified to MIL-PRF-81975 or MILPRF-57267.

Author(s):
, ; , ; , ; ,
Author Organization(s):
AERIAL REFUELING SYSTEMS ADVISORY GROUP BEAVERCREEK OH
Funding Organization(s):
DEPARTMENT OF DEFENSE WASHINGTON DC, WASHINGTON , DC
Document Type:
Technical Report/Other
Publication Date:
2023 Jan 31
Pagination:
5

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution Code:
A - Approved For Public Release
Distribution Statement: Public Release

RECORD

Collection: TRECMS
Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
refueling, air force, refueling in flight, surface roughness, couplings, rings, specifications, o rings, screw threads, databases, roughness, assembly, finishes, money, procurement
Keyword(s):
AR (Aerial Refueling), cAD (Computer Aided Design), MS (Military Standard)
Subject Categories:
Aviation Technology; Mechanical, Industrial, Civil and Marine Engineering
Creation Date:
2022 Aug 18
Update Date:
2023 Feb 06