MIL-R-7705 Revision B:1975
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
RADOME, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT)
Available format(s)
PDF
Language(s)
English
Published date
14-01-1975
Publisher
Withdrawn date
28-09-1995
€16.67
Excluding VAT
Covers general design and performance requirements for radomes used in flight vehicles, surface vehicles and fixed ground installations.
| DocumentType |
Standard
|
| Pages |
35
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
This specification covers the general design and performance requirements for radomers (see 6.3) used in flight vehicles and fixed ground installations.
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| MIL-C-83231 Revision A:1981 | Coatings, Polyurethane, Rain Erosion Resistant for Exterior Aircraft and Missile Plastic Parts (S/S by SAE-AMS-C-83231) |
| DEFSTAN 00-970(PT7)SEC2/SUPP6/5(2015) : INTERIM | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
| MIL-C-83445 Revision A:1980 | Coating System, Polyurethane, Non-Yellowing, White, Rain Erosion Resistant, Thermally Reflective (S/S by SAE-AMS-C-83445) |
| MIL-STD-877 Base Document:1968 | ANTENNA SUBSYSTEM, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF (NO S/S DOCUMENT) |
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| MIL-STD-1516 Revision B:1990 | Unified Code for Coating and Finishes for DOD Materiel (No S/S Document) |
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| MIL-I-8700 Revision A:1970 | Installation and Test of Electronic Equipment in Aircraft, General Specification for (S/S by SAE-AS8700) |
| DEFSTAN 00-970(PT7)SEC2/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 2: STRUCTURAL STRENGTH AND DESIGN FOR FLIGHT |
| MIL-T-18232 Revision B:1968 | Targets, Aerial, Powered, Design and Construction of General Specification for (No S/S Document) |
| DEFSTAN 00-970(PT7)SEC2/1(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 2: STRUCTURAL STRENGTH AND DESIGN FOR FLIGHT |
| MIL-C-18263 Revision F:1971 | Colors, Exterior, Naval Aircraft: Requirements for (S/S by MIL-STD-2161) |
| MIL A 83366 : 0 | ANTENNA ASSEMBLIES, AIRBORNE, GENERAL SPECIFICATION FOR |
| MIL-I-83456 Base Document:1974 | Installation of Segmented Lightning Diverter Strips on Aircraft Radomes, General Specification for (No S/S Document) |
| MIL P 9503 : B | PAINT, RUBBER, RIGID AND AIR SUPPORTED RADOME |
| MIL-C-9084 Revision C:1970 | Cloth, Glass, Finished, for Resin Laminates (S/S by SAE-AMS-C-9084) |
| MIL-S-9041 Revision B:1975 | Sandwich Construction; Plastic Resin, Glass Fabric Base, Laminated Facings and Honeycomb Core for Aircraft Structural and Electronic Applications |
| MIL-R-9299 Revision C:1968 | RESIN, PHENOLIC, LAMINATING (NO S/S DOCUMENT) |
| MIL-I-8500 Revision D:1980 | Interchangeability and Replaceability of Component Parts for Aerospace Vehicles |
| ASTM E 228 : 2017 : REDLINE | Standard Test Method for Linear Thermal Expansion of Solid Materials With a Push-Rod Dilatometer |
| 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-R-25042 Revision B:1967 | Resin, Polyester, High Temperature Resistant, Low Pressure Laminating |
| MIL-A-83377 Revision B:1978 | Adhesive Bonding (Structural) for Aerospace and Other Systems, Requirements for (No S/S Document) |
| L-P-383 Base Document:1967 | Plastic Material, Polyester Resin, Glass Fiber Base, Low Pressure Laminated |
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| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-C-83231 Revision A:1981 | Coatings, Polyurethane, Rain Erosion Resistant for Exterior Aircraft and Missile Plastic Parts (S/S by SAE-AMS-C-83231) |
| MIL-R-25506 Revision C:1982 | Resin Solution, Silicone, Low-Pressure Laminating |
| MIL-A-8869 Revision B:1987 | Airplane Strength and Rigidity Nuclear Weapons Effects |
| MIL F 18264 : D | FINISHES: ORGANIC, WEAPONS SYSTEM, APPLICATION AND CONTROL OF |
| MIL P 23377 : G | PRIMER COATING, EPOXY, HIGH SOLIDS |
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| FED-STD-406 Revision A:1982 | PLASTICS: METHODS OF TESTING (S/S BY - SEE CANCELLATION NOTICE FOR RECOMMENDED SUPERSEDING ASTM TEST METHODS) |
| MIL-R-7575 Revision C:1966 | Resin, Polyester, Low-Pressure Laminating |
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| MIL-STD-401 Revision B:1967 | SANDWICH CONSTRUCTIONS AND CORE MATERIALS, GENERAL TEST METHODS (S/S BY SAE-AMS-STD-401) |
| MIL-P-25518 Revision B:1981 | Plastic Materials, Silicone Resin, Glass Fiber Base, Low Pressure Laminated |
| MIL-STD-794 Revision E:1982 | PART AND EQUIPMENT, PROCEDURES FOR PACKAGING AND PACKING OF |
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| MIL-STD-490 Revision A:1985 | SpecificationPractices (S/S by MIL-STD-961) |
| MIL-Q-9858 Revision A:1963 | Quality Program Requirements (No S/S Document) |
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| MIL-C-83286 Revision B:1973 | Coating, Urethane, Aliphatic Isocyanate, for Aerospace Applications (S/S by MIL-C-85285 S/S by MIL-PRF-85285) |
| FED-STD-5 Revision F:1982 | Standard Guides for Preparation of Proposed Item Logistics Data Records |
| MIL-M-8856 Revision B:1990 | Missiles, Guided, Structural Integrity General Specification for |
| MIL-A-8860 Revision B:1987 | Airplane Strength and Rigidity, General Specification for |
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