Method for safe flight testing of high velocity interceptor miss

Ordnance – Waging war

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244 311, B64D 104, F41G 700

Patent

active

058668373

ABSTRACT:
An intercept missile testing method which includes the steps of launching a test missile threat from a first location on a substantially vertical trajectory, e.g., with a flight path angle greater than about 70.degree., towards an intercept point, and launching a test intercept missile from a second location on a substantially vertical trajectory, e.g., with a flight path angle greater than about 70.degree., towards the intercept point. The flight paths are selected so that the test intercept missile will intercept the test missile threat exoatmospherically, at an intercept (engagement crossing) angle of less than about 30.degree.. Preferably, the launch velocities and trajectories of the test intercept missile and the test missile threat are selected so that the intercept will occur exoatmospherically when the test missile threat is on a downward trajectory at a velocity of 5-8 km/sec, while the test intercept missile is on an upward trajectory at a velocity 5-9 km/sec. The first location is preferably Wake Island, Johnston Island, or Kauai, and the second location is preferably Meck Island.

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"National Missile Defense Program: When, not Whether", Defense Issues, vol. 11, No. 48, May 1996.

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