SNU-84-1-F16-REV-B-CH-1-15JUL92 Manufactured by Joint Electronics Type Designation - Order Online

Part Number:  SNU-84-1-F16-REV-B-CH-1-15JUL92
Alternate P/N:  SNU841F16REVBCH115JUL92
Item Name :  inertial navigation
CAGE Code:  80058
INC Code:  53294
Country:  USA
NCB Code:  01
FSG:  66 Instruments and Laboratory Equipment
The NSN Part SNU-84-1-F16-REV-B-CH-1-15JUL92 Inertial Navigation is ready-to-ship today! Please request a quote by filling out the form. All fields are important. The NSN number for SNU-84-1-F16-REV-B-CH-1-15JUL92 is 6605-01-455-7795. The manufacturer of this part is Joint Electronics Type Designation. A dedicated customer service executive will contact you within 15 minutes of receiving the RFQ.

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Disclaimer: This is a quotation for the goods listed above. This quotation is meant as an estimate and does not reflect a final bill or invoice. All quotations are subject to change until acceptance by ASAP Semiconductor of a binding Purchase Order, and quotations may be withdrawn or revised at the sole discretion of ASAP Semiconductor. This quotation is subject to the ASAP Semiconductor Terms & Conditions available at https://www.asapsemi.com/customer-terms-and-conditions/ . All United States Government and Department of Defense bids are quoted as CAGE code 6RE77 from ASAP Semiconductor’s Anaheim, California facility. Any quotation from ASAP Semiconductor without 6RE77 is void.

Characteristics Data of NSN 6605-01-455-7795, 6605014557795

MRCCriteriaCharacteristic
ABMKOVERALL WIDTH6.750 INCHES NOMINAL
SR-1SPEC/STD CONTROLLING DATA
FEATSPECIAL FEATURESRECIEVES 26 V, 400 HZ SINGLE PHASE SYNCHRO REFERENCE POWER; AIRCRAFT 28 VDC DISCRETE POWER EXCLUDING BATTERY BACK UP POWER
ABKWOVERALL HEIGHT7.625 INCHES NOMINAL
SUPPIII SUPPLEMENTARY FEATURESELECTROSTATIC DISCHARGE SENSITIVE
AGAVIII END ITEM IDENTIFICATIONF-16 A TO D MODEL AIRCRAFT
ACDCCURRENT TYPEDC
ABHPOVERALL LENGTH15.187 INCHES NOMINAL
ELECVOLTAGE IN VOLTS115.0 AND 200.0
SR-1MANUFACTURERS CODE81349
FTLDIII FUNCTIONAL DESCRIPTIONCAPABLE OF DETERMINING POSITION, VELOCITY, HEADING, ACCELERATIONS, BODY RATES, AND ATTITUDE IN THE AUTONOMOUS MODE FROM TAKE OFF TO LANDING AFTER A GROUND ALIGNMENT IN THE FOLLOWING MODES: GYROCOMPASS, STORED HEADING, BEST AVAILABLE TRUE HEADING
FREQFREQUENCY IN HERTZ400.0
SR-1NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCESNU 84-1/F16 REV B CH 1 15JUL92

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