Contact arrangements materials and finishes dimensions PCB layout panel cutout

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Contact arrangements materials and finishes dimensions PCB layout panel cutout SuperFly to AlphaLink flex jumper Superfly to AlphaLink Flex Jumpers Glenair Series 88 SuperFly Cordsets represent a perfect storm of high-performance contacts, shells, wires, termination and mating technologies. SuperFly combines the weight-saving and performance advantages of nanominiature contacts in a precision package made to order for battlefield and other high-performance applications. Now available in turnkey flex jumper format for easy integration in printed circuit board applications, each SuperFly jumper ships with rugged Polyimide-based flex terminated to your choice of threaded or quick disconnect coupling nanominiature flex jumpers SuperFly and an AlphaLink SL board level connector. Recommended SuperFly I/O to AlphaLink Contact Arrangements* 1 2 3 5 6 7 B7N 1 2 3 5 6 8 9 10 C10N 1 3 4 7 8 12 13 16 17 19 E19N 1 4 5 9 10 13 14 18 19 22 F22N 4 1 8 5 5 1 10 6 10 1 20 11 14 1 28 15 8 Contacts 10 Contacts 20 Contacts 28 Contacts 3 8 14 19 25 1 30 2 31 7 13 18 24 29 1 4 5 9 10 15 16 22 23 28 29 33 34 37 1 5 6 11 12 18 19 26 27 33 34 39 40 44 To optimize the 40-contact AlphaLink board level connector, 40 contacts of a 44-contact size SuperFly connector can be used. G31N H37N J44N 16 1 32 17 32 Contacts 20 1 40 21 40 Contacts * These are recommended contact arrangements only, but do offer best availability. Contacts are mapped 1-to-1 from I/O to B/L connector (unused B/L contacts not connected). For alternative wire schedules, please consult factory. 16 2013 Glenair, Inc 1211 Air Way, Glendale, CA 91201 818-247-6000 www.glenair.com U.S. CAGE code 06324

Contact arrangements materials and finishes dimensions PCB layout panel cutout.150 BB Ø.042 Typ. Pads 4X R.015 Max 1 10.050.050 Typ 11 20.025 2x Ø.080 Mounting Holes ø B C Recommended PCB Layout (See Table V) Recommended Panel Cutout (See Table IV) Table I - I/O Material/Finish Sym Material Finish M Electroless Nickel ZR Black Zinc-Nickel over Aluminum Alloy Electroless Nickel MT Nickel-PTFE NF Olive drab over Cadmium ZC Black Zinc Cobalt ZK Stainless Steel Passivate ZMT Nickel Teflon Table III - Available I/O Insert Arrangement and B/L Assembly Pairs* Ins. Arr. I/O Contact B/L Qty Layout B7N Nano 7 8 C10N Nano 10 10 E19N Nano 19 20 F22N Nano 22 28 G31N Nano 31 32 H37N Nano 37 40 J44N Nano 44 40 * Contacts mapped 1-to-1 from I/O to B/L connector (unused B/L contacts not connected). For alternative wire schedules, please consult factory. Table IV - I/O Connector Panel Cutout imensions Shell Ø A Ø B C Flats B.392 (10.0).283 (7.2).241 (6.1) C.412 (10.5).305 (7.7).261 (6.6) E.451 (11.5).344 (8.7).300 (7.6) F.471 (12.0).364 (9.2).320 (8.1) G.490 (12.4).383 (9.7).340 (8.6) H.530 (13.5).349 (8.9).379 (9.6) J.569 (14.5).459 (11.7).418 (10.6) Table V - B/L Connector imensions Layout AA BB 4.527 (13.4).350 (8.9) 8.627 (15.9).450 (11.4) 10.677 (17.2).500 (12.7) 16.827 (21.0).650 (16.5) 20.927 (23.5).750 (19.1) 28 1.127 (28.6).950 (24.1) 32 1.227 (31.2) 1.050 (26.7) 40 1.427 (36.2) 1.250 (31.8) 17 2013 Glenair, Inc 1211 Air Way, Glendale, CA 91201 818-247-6000 www.glenair.com U.S. CAGE code 06324

SuperFly quick-disconnect rear-panel-mount 880-034 Series 88 superfly Input/Output (I/O) qdc receptacle to alphalink SL spring loaded contact Board Level (B/L) connector How To Order 880-034 Sample Part Number 880-034R A -F22N -M -2 T -6 S Series / Basic Part No. I/O Insert Configuration I/O Shell / Contact Arrangement Series 88 SuperFly QC I/O receptacle to Series 171 AlphaLink SL A = Unshrouded contacts (e.g. Nano socket) B = Shrouded contacts (e.g. Nano TwistPin) B7N, C10N, E19N, F22N, G31N, H37N, J44N (See Contact Arrangements and Table III, page 16 17) I/O Shell Material/Finish (See Table I) AlphaLink Finish 2 = Nickel 5 = Gold AlphaLink Hardware Option T = Threaded thru hole Omit for thru hole Assembly Length (L) 3 = 3.00 ±.05 inches 6 = 6.00 ±.05 inches 12 = 12.00 ±.05 inches Optional Shielding S = With shielding Omit for none Table I - I/O Material/Finish Sym Material Finish M Electroless Nickel ZR Black Zinc-Nickel over Aluminum Alloy Electroless Nickel MT Nickel-PTFE NF Olive drab over Cadmium ZC Black Zinc Cobalt ZK Stainless Steel Passivate ZMT Nickel Teflon materials and finishes B/L connector shell: Aluminum alloy. I/O shell, jam nut: See Table I Insulator: Liquid crystal polymer or equivalent Seals, grommet, O-ring: Fluorosilicone or equivalent Contacts: Copper Alloy/Gold Plated Potting: Epoxy Notes Input/Output Series 88 SuperFly quick-disconnect receptacle: I/O connector will mate with all plug QC SuperFly connectors with same polarization and opposite insert configuration. Insert arrangement per 889-001. See page 16 and 17, Table III for available arrangements. Unshrouded configurations are opposite of shrouded. Contacts mapped 1-to-1 from I/O to B/L connector (unused B/L contacts not connected). For alternative wire schedules, please consult factory. See 880-032 for other connector dimensions Board Level AlphaLink SL connector: B/L AlphaLink SL connectors are built in accordance with Glenair drawing 171-134-02 B/L connectors are paired with I/O connectors as shown on Table III Flex Performance: Shielding - EMI shielding film. Bend radius is 6 to 10 times the flex thickness. Typical flex will be.01 ±.005 thick, rugged, potted, polyimidebased flex. Flex cables are terminated from the I/O connector to the B/L connector on a 1 to 1 connection (unused B/L contacts are not connected) Workmanship shall be IAW IPC-6013, Class 2. Consult factory for more options and/or special designs and requirements 18 2013 Glenair, Inc 1211 Air Way, Glendale, CA 91201 818-247-6000 www.glenair.com U.S. CAGE code 06324

SuperFly quick-disconnect rear-panel-mount 880-034.69 Max.35 Max Ø A I/O L ±.05 Pos 1 BB AA.183.258 Ø.021/.017 Typ B/L Alpha Link SLC.032 ±.015 Typ Table IV - I/O Connector imensions Shell Ø A Ø B C Flats B.392 (10.0).283 (7.2).241 (6.1) C.412 (10.5).305 (7.7).261 (6.6) E.451 (11.5).344 (8.7).300 (7.6) F.471 (12.0).364 (9.2).320 (8.1) G.490 (12.4).383 (9.7).340 (8.6) H.530 (13.5).349 (8.9).379 (9.6) J.569 (14.5).459 (11.7).418 (10.6) Table V - B/L Connector imensions Layout AA BB 4.527 (13.4).350 (8.9) 8.627 (15.9).450 (11.4) 10.677 (17.2).500 (12.7) 16.827 (21.0).650 (16.5) 20.927 (23.5).750 (19.1) 28 1.127 (28.6).950 (24.1) 32 1.227 (31.2) 1.050 (26.7) 40 1.427 (36.2) 1.250 (31.8) 19 2013 Glenair, Inc 1211 Air Way, Glendale, CA 91201 818-247-6000 www.glenair.com U.S. CAGE code 06324

SUPERFLY TO ALPHALINK FLEX JUMPERS SuperFly threaded rear-panel-mount 881-021 SERIES 88 SUPERFLY INPUT/OUTPUT (I/O) THREAE RECEPTACLE TO ALPHALINK SL SPRING LOAE CONTACT BOAR LEVEL (B/L) CONNECTOR How To Order 881-021 Sample Part Number 881-021R A -F22N -M -2 T -6 S Series / Basic Part No. I/O Insert Configuration I/O Shell / Contact Arrangement Series 88 SuperFly QC I/O receptacle to Series 171 AlphaLink SL A = Unshrouded contacts (e.g. Nano socket) B = Shrouded contacts (e.g. Nano TwistPin) B7N, C10N, E19N, F22N, G31N, H37N, J44N (See Contact Arrangements and Table III, page 16 17) I/O Shell Material/Finish (See Table I) AlphaLink Finish 2 = Nickel 5 = Gold AlphaLink Hardware Option T = Threaded thru hole Omit for thru hole Assembly Length (L) 3 = 3.00 ±.05 inches 6 = 6.00 ±.05 inches 12 = 12.00 ±.05 inches Optional Shielding S = With shielding Omit for none Table I - I/O Material/Finish Sym Material Finish M Electroless Nickel ZR Black Zinc-Nickel over Aluminum Alloy Electroless Nickel MT Nickel-PTFE NF Olive drab over Cadmium ZC Black Zinc Cobalt ZK Stainless Steel Passivate ZMT Nickel Teflon MATERIALS AN FINISHES B/L connector shell: Aluminum alloy. I/O shell, jam nut: See Table I Insulator: Liquid crystal polymer or equivalent Seals, grommet, O-ring: Fluorosilicone or equivalent Contacts: Copper Alloy/Gold Plated Potting: Epoxy NOTES Input/Output Series 88 SuperFly threaded receptacle: I/O connector will mate with all plug threaded SuperFly connectors with same polarization and opposite insert configuration. Insert arrangement per 889-001. See page 16 and 17, Table III for available arrangements. Unshrouded configurations are opposite of shrouded. Contacts mapped 1-to-1 from I/O to B/L connector (unused B/L contacts not connected). For alternative wire schedules, please consult factory. See 881-019 for other connector dimensions Board Level AlphaLink SL connector: B/L AlphaLink SL connectors are built in accordance with Glenair drawing 171-134-02 B/L connectors are paired with I/O connectors as shown on Table III Flex Performance: Shielding - EMI shielding film. Bend radius is 6 to 10 times the flex thickness. Typical flex will be.01 ±.005 thick, rugged, potted, polyimidebased flex. Flex cables are terminated from the I/O connector to the B/L connector on a 1 to 1 connection (unused B/L contacts are not connected) Workmanship shall be IAW IPC-6013, Class 2. Consult factory for more options and/or special designs and requirements 20 2013 Glenair, Inc 1211 Air Way, Glendale, CA 91201 818-247-6000 www.glenair.com U.S. CAGE code 06324

SuperFly threaded rear-panel-mount 881-021.800 Max.610 Max Ø A I/O L ±.05 Pos 1 BB AA.183 Ø.021/.017 Typ B/L Alpha Link SLC.258.032 ±.015 Typ Table IV - I/O Connector imensions Shell Ø A Ø B C Flats B.392 (10.0).283 (7.2).241 (6.1) C.412 (10.5).305 (7.7).261 (6.6) E.451 (11.5).344 (8.7).300 (7.6) F.471 (12.0).364 (9.2).320 (8.1) G.490 (12.4).383 (9.7).340 (8.6) H.530 (13.5).349 (8.9).379 (9.6) J.569 (14.5).459 (11.7).418 (10.6) Table V - B/L Connector imensions Layout AA BB 4.527 (13.4).350 (8.9) 8.627 (15.9).450 (11.4) 10.677 (17.2).500 (12.7) 16.827 (21.0).650 (16.5) 20.927 (23.5).750 (19.1) 28 1.127 (28.6).950 (24.1) 32 1.227 (31.2) 1.050 (26.7) 40 1.427 (36.2) 1.250 (31.8) 21 2013 Glenair, Inc 1211 Air Way, Glendale, CA 91201 818-247-6000 www.glenair.com U.S. CAGE code 06324