MIL-HDBK-694 Revision A:1966
Withdrawn
Withdrawn
Aluminum and Aluminum Alloys (No S/S Document)
Available format(s)
PDF
Language(s)
English
Published date
12-15-1966
Publisher
Withdrawn date
07-27-1994
US$20.00
Excluding Tax where applicable
| DocumentType |
Standard
|
| Pages |
108
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
The purpose of this handbook is to provide, in condensed form, technical information and data of direct usefulness to design engineers.
| MIL-A-23121 Revision C:1970 | Aircrew Environmental, Escape and Survival Cockpit Capsule System General Specification for (No S/S Document) |
| MIL-A-81973 Base Document:1974 | Aircrew Automated Escape Systems, Test Vehicles for Ground Track Performance Testing, Rocket and/or Jet Engine Propelled, General Specification for (No S/S Document) |
| MIL-R-85880 Base Document:1988 | ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL-HDBK-772 Base Document:1981 | Military Packaging Engineering (No S/S Document) |
| MIL-S-18471 Revision G:1983 | System, Aircrew Automated Escape, Ejection Seat Type, General Specification For |
| DOD HDBK 270 : 0 | METALLIC MATERIALS, MAGNETIC PERMEABILITY AND ELECTRICAL CONDUCTIVITY, CHARACTERISTICS OF (METRIC) |
| MIL-I-85889 Base Document:1988 | IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL-HDBK-270 Revision A:1991 | Metallic Materials, Magnetic Permeability and Electrical Conductivity, Characteristics of (Metric) |
| MIL-P-83126 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
Summarise
US$20.00
Excluding Tax where applicable
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