Defence Standards: Recent submissions
Now showing items 821-840 of 43216
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MIL-I-24728/5
Abstract: This specification is approved for use by all Departments and Agencies of the Department of Defense.
The requirements for acquiring the product described herein shall consist of this specification sheet and the issue ... -
A-A-1439B
Abstract: This commercial item description (CID) covers phenolic type disinfectant-detergent. The disinfectant-detergent described herein is intended for use as a general purpose cleaner and disinfectant for hard surfaces such as ... -
NATO STANAG 7184
Abstract: AIM
The aim of this agreement is to achieve a common series of attainable standards and management objectives to minimise the probability of a loss of military capability caused by an outbreak of fire or explosion ... -
NASA-LLIS-0222
Abstract: Description of Driving Event:
Some of the original equipment manufacturers are not providing sufficient support for out-ofproduction parts. NASA and its contractors have evolved good systems for ...Subject(s) : Hardware , Launch Vehicle , Logistics , -
NACA-TN-1110
Abstract: INTRODUCTION
Tests were made in the Langley two-dimensional low-turbulence tunnels of an airfoil section equipped with a double slotted flap designed for application to a fighter type airplane. Preliminary design of ... -
NASA-TN-D-6909
Abstract: An investigation was conducted in the Langley full-scale tunnel to determine the dynamic stability derivatives in pitch, roll, and yaw over an angle-of-attack range of -5 deg to 90 deg for a variable-sweep fighter configuration ...Subject(s) : AERODYNAMIC , AIRCRAFT , CHARACTERISTICS , CONFIGURATIONS , DERIVATIVES , FIGHTER , STABILITY , SWEEP , TESTS , TUNNEL , VARIABLE , WIND , WINGS , -
NACA-TN-1284
Abstract: INTRODUCTION
The problem of producing airplanes capable of flight speeds equal to and greater that the speed of sound with a reasonable expenditure of power has been studied by airplane designers for some time. In order ...Subject(s) : AIRFOILS , ASPECT , CARRIED , CHAR , DRAG , EDGE , EXTENDED , FLAPS , LEADING , LMAL , LONGITUDINAL , LOW , MOMENTS , MPH , NACA , NAVY , RATIO , SLOTS , STABILITY , SWEPTBACK , TESTS , TIP , TIPS , TUNNEL , WIND , WING , WINGS , WORK , -
MIL-M-38510/347A
Abstract: This specification covers the detail requirements for monolithic silicon, advanced Schottky TTL, 8-bit identity comparator, logic gate microcircuits. Two product assurance classes and a choice of case outlines and lead ... -
NATO AMOVP-4(A)
Abstract: AIM
The aim of this allied publication is to give in ONLY ONE document the procedure and all technical rules applicable to the loading/unloading and the transport of military equipment on railway wagons. -
NASA-LLIS-1281
Abstract: Description of Driving Event:
The Project underwent several reviews throughout its lifecycle. In general, these reviews helped the Project maintain its course and manage its resources effectively and ...Subject(s) : Administration/Organization , Policy & Planning , -
NATO STANAG 6001
Abstract: AIM
The aim of this agreement is to provide NATO Forces with a table describing language proficiency levels.

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