Accession Number:

AD0831567

Title:

MISSILE TRACKING FROM SHOCK RECORDINGS,

Personal Author(s):

Corporate Author:

NAVAL ORDNANCE LAB WHITE OAK MD

Report Date:

1968-03-01

Abstract:

Equations are developed for determining the speed and direction of motion of a supersonic missile in terms of the times of arrival of the shock at various microphones. Three or more microphones must be placed along the x, y and z axes at each of three or more stations. Author

Pages:

0015

Descriptors:

Identifiers:

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Communities Of Interest:

File Size:

0.00MB

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