Defence Standards: Recent submissions
Now showing items 1181-1200 of 43216
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NACA-RM-A52L04 REV A
Abstract: INTRODUCTION
In the classical study of the longitudinal motion of an aircraft, it is usually found that the motion resulting from a small equilibrium destroying disturbance consist of two modes: one, a lightly damped, ... -
MIL-PRF-12048E VALID NOTICE 1
Abstract: This specification covers a petroleum testing kit for ground fuels. The equipment is used to perform American Petroleum Institute (API) and American Society for Testing and Materials (ASTM) tests for temperature determination, ...Subject(s) : Contaminants , Distillation , Flash point , Free water , Fuel , -
W-L-101/43A
Abstract: This specification sheet was approved by the Commissioner, Federal Supply Service, General Services Administration, for the use of all Federal agencies.
(This specification sheet forms a part of the latest issue of ... -
DODD 5230.20(D) 06/22/05
Abstract: APPLICABILITY AND SCOPE
This Directive applies to the Office of the Secretary of Defense (OSD), the Military Departments, the Chairman of the Joint Chiefs of Staff, the Combatant Commands, the Office of Inspector ... -
SMD-5962-77046 REV G
Abstract: This drawing describes device requirements for MIL-STD-883 compliant, non-JAN class level B microcircuits in accordance with MIL-PRF-38535, appendix A. Intended Use: Microcircuits conforming to this drawing ... -
COMDTINST 4105.7
Abstract: APPLICABILITY. This Instruction applies to all Coast Guard offices and activities involved with the acquisition, planning and management of the support of platforms, systems, and equipment. This Instruction shall ... -
SMD-5962-95707
Abstract: This drawing forms a part of a one part - one part number documentation system (see 6.6 herein). This drawing describes device requirements for hybrid microcircuits to be processed in accordance with MIL-PRF-38534. ... -
NACA-TR-971
Abstract: The stability derivatives valid for a limited range of supersonic speeds are presented for a series of sweptback wings tapered to a point with sweptback or sweptforward trailing edges. These wings were derived by ...Subject(s) : AERODYNAMIC , AIRCRAFT , COMPUTATIONAL , DELTA , DISTRIBUTION , DYNAMICS , EDGES , EFFECT , FLOW , FLUID , LOADING , PARTS , PRESSURE , STABILITY , SUPERSONIC , SWEEP , SWEPT , THIN , TRAILING , WING , WINGS , -
SMD-5962-93221 REV A
Abstract: This drawing documents two product assurance class levels consisting of high reliability (device classes Q and M) and space application (device class V). A choice of case outlines and lead finishes are available and are ...

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