Exemples d'utilisation de Usable in the systems en Anglais et leurs traductions en Français
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Official
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Colloquial
Usable in the systems specified in 1.A. or 19.A.1.
Analogue-to-digital converters, usable in the systems specified in 6-1.A.
Usable in the systems specified in 1.A. or 19.A.1.
High energy density materials, usable in the systems specified in 6-1.A.
Liquid and slurry propellant(including oxidisers) control systems, andspecially designed components therefor, usable in the systems specified in 6-1.A.
Maraging steels, usable in the systems specified in 6-1.A.
Staging mechanisms, separation mechanisms, andinterstages therefor, usable in the systems specified in 1.A.
Complete subsystems usable in the systems specified in 1.A., as follows.
Staging mechanisms, separation mechanisms, andinterstages therefor, usable in the systems specified in 1.A.
Complete subsystems usable in the systems specified in 6-1.A., as follows.
Rocket motor cases,'insulation' components andnozzles therefor, usable in the systems specified in 6-1.A.
Analogue-to-digital converters, usable in the systems specified in 1.A., having any of the following characteristics.
Re-entry vehicles, andequipment designed or modified therefor, usable in the systems specified in 6-1.A.
Thrust vector control sub-systems, usable in the systems specified in 1.A., except as providedin the Note below 2.A.1.
Weapon or warhead safing, arming,fuzing, and firing mechanisms, usable in the systems specified in 6-1.A.
All types of gyros usable in the systems specified in 1.A., 19.A.1 or 19.A.2., with a rated'drift rate''stability' of less than 0.5 degrees(1 sigma or rms) per hour in a 1 g environment, and specially designed components therefor.
Analogue-to-digital converters, usable in the systems specified in 1.A.
Guidance sets", usable in the systems specified in 1.A., capable of achieving system accuracy of 3.33% or less of the"range"(e.g. a"CEP" of 10 km or less at a"range" of 300 km), except as provided in the Note below 2.A.1. for those designed for missiles with a"range" under 300 km or manned aircraft;
Rocket propulsion subsystems, usable in the systems specified in 1.A., as follows.
Solid propellant rocket motors,hybrid rocket motors or liquid propellant rocket engines, usable in the systems specified in 6-1.A.