 | United States. Congress. Senate. Committee on Armed Services - Legislative hearings - 1979 - 1662 pages
...can be covered by the missile in its standard design mode flying until fuel exhaustion, detenninied by projecting its flight path onto the Earth's sphere...is held back. Projecting its flight path onto the Earth's sphere. — The distance measured would be that measured by the odometer of an automobile driven... | |
 | United States. Arms Control and Disarmament Agency - Arms control - 1979 - 924 pages
...can be covered by the missile in its standard design mode flying until fuel exhaustion, determined by projecting its flight path onto the earth's sphere from the point of launch to the point of impact (Second Agreed Statement). The key features of this definition are as follows: • Standard design... | |
 | Government publications - 1987 - 634 pages
...can be covered by the missile in its standard design mode flying until fuel exhaustion, determined by projecting its flight path onto the earth's sphere from the point of launch to the point of impact. GLBMs or GLCMs that have a range capability equal to or in excess of 500 kilometers but not in excess... | |
 | Nuclear disarmament - 304 pages
...can be covered by the missile in its standard design mode flying until fuel exhaustion, determined by projecting its flight path onto the Earth's sphere from the point of launch to the point of impact. Third Agreed Statement. lf an unmanned, self-propelled, guided vehicle which sustains flight through... | |
 | United States. Congress. Senate. Committee on Foreign Relations - Arms control - 1979 - 634 pages
...onto the earth's sphere from the point of launch to the point of impact (Second Agreed Statement). The key features of this definition are as follows...held back. — Projecting its flight path onto the earth's sphere. The distance measured would be that measured by the odometer of an automobile driven... | |
 | United States. Congress. Senate. Committee on Foreign Relations - Arms control - 1979 - 596 pages
...that it was done in a straight line, which obviously does not mean its range then could be projected onto the earth's sphere from the point of launch to the point of impact and come up with a true measure of range. That, apparently, is what was at odds during the negotiating... | |
 | United States. President - Arms control - 1981 - 514 pages
...can be covered by the missile in its standard design node flying until fuel exhaustion, determined by projecting its flight path onto the Earth's sphere from the point of launch to the point of impact. Monitoring MRASM Range Capability. [Deleted] For instance, cruise missile ranges are altituderelated;... | |
 | United States. President (1981-1989 : Reagan) - Presidents - 1982 - 940 pages
...can be covered by the missile in its standard design mode flying until fuel exhaustion, determined by projecting its flight path onto the earth's sphere from the point of launch to the point of impact. GLBMs or GLCMs that have a range capability equal to or in excess of 500 kilometers but not in excess... | |
 | Coit D. Blacker, Stanford Arms Control Group - Political Science - 1984 - 526 pages
...can be covered by the missile in its standard design mode flying until fuel exhaustion, determined by projecting its flight path onto the Earth's sphere from the point of launch to the point of impact. Third Agreed Statement. If an unmanned, self-propelled, guided vehicle which sustains flight through... | |
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The range of which a cruise missile is capable is the maximum distance which can be covered by the missile in its standard design mode flying until fuel exhaustion, determined by projecting its flight path onto the Earth's sphere from the point of launch... 
