MIL-R-7705 Revision B:1975
Withdrawn
Withdrawn
RADOME, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT)
Available format(s)
PDF
Language(s)
English
Published date
01-14-1975
Publisher
Withdrawn date
09-28-1995
US$20.00
Excluding Tax where applicable
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Withdrawn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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| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| 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) |
| DEFSTAN 07-85(PT1)/3(2006) : 2006 | DESIGN REQUIREMENTS FOR WEAPONS AND ASSOCIATED SYSTEMS - PART 1: MANDATORY DESIGN REQUIREMENTS |
| MIL-STD-1516 Revision B:1990 | Unified Code for Coating and Finishes for DOD Materiel (No S/S Document) |
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| MIL C 85629 : A (1) | CONTROL MONITOR SET GUIDED WEAPON, AN/AWW-13 |
| MIL-I-8673 Base Document:1955 | Installation and Test of Aircraft Flexible Weapons Systems (No S/S Document) |
| DEFSTAN 00-970(PT7)SEC2/3(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 2: STRUCTURAL STRENGTH AND DESIGN FOR FLIGHT |
| 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 |
| MIL C 8073 : D | CORE MATERIAL, PLASTIC HONEYCOMB, LAMINATED CLASS FABRIC BASE, FOR AIRCRAFT STRUCTURAL AND ELECTRONIC APPLICATIONS |
| 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 |
| MIL-P-9400 Revision C:1991 | Plastic Laminate and Sandwich Construction Parts and Assembly, Aircraft Structural, Process Specification Requirements |
| 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 |
| MIL C 22750 : F | COATING, EPOXY, VOC-COMPLIANT |
| 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 |
| MIL-P-25515 Revision C:1968 | PLASTIC MATERIALS, PHENOLIC RESIN, GLASS-FIBER BASE, LAMINATED |
| MIL-STD-100 Revision G:1997 | ENGINEERING DRAWINGS (S/S BY ASME-Y14.100, ASME-Y14.24, ASME-Y14.35M, AND ASME-14.34M) |
| MIL C 8087 : C | CORE MATERIAL, FOAMED IN PLACE, URETHANE TYPE |
| 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) |
| FED-STD-102 Revision B:1963 | PRESERVATION, PACKAGING, AND PACKING LEVELS (S/S BY MIL-P-116 AND MIL-STD-2073) |
| MIL-R-9300 Revision B:1968 | Resin, Epoxy, Low-Pressure Laminating |
| MIL C 81773 : C | COATING, POLYURETHANE, ALIPHATIC, WEATHER RESISTANT |
| MIL-B-5087 Revision B:1964 | Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464) |
| 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 |
| MIL-S-25392 Revision B:1968 | Sandwich Construction, Plastic Resin, Glass Fabric Base, Laminated Facings and Polyurethane Foamed-in-Place Core, For Aircraft Structural Applications |
Summarise
US$20.00
Excluding Tax where applicable
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