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Timing Control SystemA timing control system is disclosed which is particularly useful in connection with simulated mortar shells. Special circuitry is provided to assure that the shell does not over shoot, but rather detonates early in case of an improper condition; this ensures that ground personnel will not be harmed by a delayed detonation. The system responds to an externally applied frequency control code which is configured to avoid any confusion between different control modes. A premature detonation routine is entered in case an improper time-setting signal is entered, or if the shell is launched before completion of the time-setting sequence. Special provisions are also made for very early launch situations and improper detonator connections. An alternate abort mode is provided to discharge the internal power supply without a detonation in a manner that can be externally monitored, thereby providing a mechanism for non-destructive testing. The abort mode also accelerates the timing function for rapid testing.
Document ID
19880015479
Acquisition Source
Legacy CDMS
Document Type
Other - Patent Application
Authors
Wiker, Gordon A.
(NASA Pasadena Office CA, United States)
Wells, George H., Jr.
(Jet Propulsion Lab. California Inst. of Tech., Pasadena., United States)
Date Acquired
September 5, 2013
Publication Date
September 23, 1987
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
NAS 1.71:NPO-16882-1-CU
Patent Application Number: US-PATENT-APPL-SN-154711
Report Number: NAS 1.71:NPO-16882-1-CU
Patent Number: NASA-CASE-NPO-16882-1-CU
Accession Number
88N24863
Funding Number(s)
CONTRACT_GRANT: NAS7-918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-NPO-16882-1-CU
Patent Application
US-PATENT-APPL-SN-154711
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