NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Igniter heater EMI transient testTesting to evaluate Redesigned Solid Rocket Motor igniter heater electromagnetic interference (EMI) effects on the Safe and Arm (S and A) device was completed. It was suspected that EMI generated by the igniter heater and it's associated electromechanical relay could cause a premature firing of the NASA Standard Initiators (NSIs) inside the S and A. The maximum voltage induced into the NSI fire lines was 1/4 of the NASA specified no-fire limit of one volt (SKB 26100066). As a result, the igniter heaters are not expected to have any adverse EMI effects on the NSIs. The results did show, however, that power switching causes occasional high transients within the igniter heater power cable. These transients could affect the sensitive equipment inside the forward skirt. It is therefore recommended that the electromechanical igniter heater relays be replaced with zero crossing solid state relays. If the solid state relays are installed, it is also recommended that they be tested for EMI transient effects.
Document ID
19890019195
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cook, M.
(Morton Thiokol Brigham City, UT, United States)
Date Acquired
September 6, 2013
Publication Date
June 9, 1989
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:183743
NASA-CR-183743
TWR-18915
Report Number: NAS 1.26:183743
Report Number: NASA-CR-183743
Report Number: TWR-18915
Accession Number
89N28566
Funding Number(s)
CONTRACT_GRANT: NAS8-30490
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available