MIL R 25532 : A
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR
Withdrawn date
01-06-1996
Publisher
Sorry this product is not available in your region.
Sets forth standard requirements for rocket motors for aeronautical vehicles.
| Committee |
FSC 1337
|
| DocumentType |
Standard
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| MIL-R-25536 Revision A:1959 | ROCKET MOTOR, AERONAUTICAL, ACCEPTANCE TEST FOR |
| MIL R 25533 : A | ROCKET MOTOR, AERONAUTICAL, MODEL SPECIFICATION FOR (OUTLINE AND INSTRUCTIONS FOR PREPARATION) |
| MIL-R-25535 Revision A:1959 | ROCKET MOTOR, AERONAUTICAL, PRELIMINARY FLIGHT RATING TEST FOR |
| MIL R 25534 : A NOTICE 1 | ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR |
| SAE AMS 2650 : 1992 | FLUOROSCOPIC X-RAY INSPECTION |
| MIL R 25533 : A | ROCKET MOTOR, AERONAUTICAL, MODEL SPECIFICATION FOR (OUTLINE AND INSTRUCTIONS FOR PREPARATION) |
| PPP-C-96 Revision E:1992 | CAN, METAL, 28 GAGE AND LIGHTER |
| SAE AMS 2645 : 1995 | FLUORESCENT PENETRANT INSPECTION |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| MIL-P-7105 Revision B:1965 | PIPE THREADS, TAPER, AERONAUTICAL NATIONAL FORM, SYMBOL ANPT. GENERAL REQUIREMENTS FOR |
| PPP-B-636 Revision J:1981 | BOX, SHIPPING, FIBERBOARD |
| MIL-H-25475 Revision B:1971 | HYDRAULIC SYSTEM, MISSILE, DESIGN, INSTALLATION TESTS AND DATE REQUIREMENTS, GENERAL REQUIREMENTS FOR |
| MIL I 6866 : B | INSPECTION, PENETRANT METHOD OF |
| MIL-E-25499 Revision C:1970 | ELECTRICAL SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION OF, GENERAL REQUIREMENTS FOR |
| MIL-T-5021 Revision D:1969 | MILITARY SPECIFICATION. TESTS; AIRCRAFT AND MISSILE WELDING OPERATORS' QUALIFICATION |
| MIL-R-25535 Revision A:1959 | ROCKET MOTOR, AERONAUTICAL, PRELIMINARY FLIGHT RATING TEST FOR |
| MIL-B-13239 Revision G:1977 | BARRIER MATERIAL, WATER PROOFED, FLEXIBLE, ALL TEMPERATURE, HEAT SEALABLE |
| MIL-C-25731 Revision A:1968 | CRATES, WOOD, FOR DOMESTIC AND OVERSEAS SHIPMENT OF AIRFRAME COMPONENTS (2,OOO POUND MAXIMUM NET LOAD) |
| MIL P 7936 : LATEST | PARTS AND EQUIPMENT, AERONAUTICAL, PREPARATION FOR DELIVERY |
| MIL-I-6868 Revision E:1976 | INSPECTION PROCESS, MAGNETIC PARTICLE |
| MIL R 25534 : A NOTICE 1 | ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR |
| MIL-H-8775 Revision D:1976 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
| MIL-M-8555 Revision C:1984 | MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
| MIL-R-25536 Revision A:1959 | ROCKET MOTOR, AERONAUTICAL, ACCEPTANCE TEST FOR |
| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF |
| MIL E 7894 : A | |
| MIL-H-5440 Revision H:1993 | HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
| MIL I 6865 : LATEST | INSPECTION, RADIOGRAPHIC |
| PPP-B-621 Revision D:1981 | BOXES, WOOD, NAILED AND LOCK CORNER |
| MIL-P-8564 Revision D:1970 | PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
| MIL X 6141 : LATEST | X-RAY LABORATORY, PROCEDURE FOR CERTIFICATION |
| MIL-S-7742 Revision D:1991 | SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR |
| SAE AMS 2640 : 1996 | MAGNETIC PARTICLE INSPECTION |
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