SOW_NAWC_80084432_SlipRing_A12.pdf
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- Slip Ring
- Solicitation number
- N6893624Q0135
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This document is a Statement of Work (SOW) for a slip ring requirement for the Naval Air Warfare Center Weapons Division (NAWCWD) Common Core Radar (CCR) program. The SOW defines the technical specifications for the slip ring, which will have three differential low voltage channels and one differential high voltage channel. The slip ring must be a current design and proven product that meets enhanced performance requirements.
The related federal contract opportunity is a pre-solicitation notice for the procurement of 13 slip ring AC7466 and 4 harnessed AC6907-1 units on an other than full and open competition basis. The procurement will be a Firm Fixed Price (FFP) commercial contract with Moog Inc. Blacksburg Operations. The government is accepting written responses from other firms that believe they can fulfill the requirement by October 3, 2024. The Naval Air Warfare Center is the procuring agency for this effort.
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2 / 9 UNCLASSIFIED
UNCLASSIFIED
Type 20 Radar
SLIP RING A12
Statement of Work July 2024
Document Number: 80084432
Revision C
Prepared by Naval Air Warfare Center Weapons Division (NAWCWD)
Weapons Control and Integration Branch Code D55J300 STOP 6633
China Lake, CA 93555-6110
DISTRIBUTION STATEMENT D: Distribution authorized to the Department of Defense and U.S. DoD contractors only; Critical Technology, March 2010. Other U.S. requests shall be referred to COMNAVSEASYSCOM (SEA 09P3) and PEO SUB (PMS435) and NAVSEA 09P3 or higher DOD authority.
WARNING: This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec. 2751, et.
Seq.) or the Export Administration Act of 1979, as amended, Title 50, U.S.C., App. 2401 et seq. violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of OPVAVINST 5510.161.
DESTRUCTION NOTICE – Classified Information, destroy in accordance with the DOD 5220.22-M, National Industrial Security Program Operating Manual. Unclassified limited documents, (e.g., FOUO, distribution statement control) destroy by any methods that will prevent disclosure of contents or reconstruction of the document.
3 / 9 UNCLASSIFIED
4 / 9 UNCLASSIFIED
1. OBJECTIVE
Naval Air Warfare Center Weapons Division (NAWCWD) requires high quality slip rings for the Common Core Radar (CCR) program. A current design and proven product must be updated to meet enhanced performance requirements. This specification and reference 2.1 define the Slip Ring required specification. Other references in section 2.0 and as indicated on reference 2.1 are applied as defined within this specification or reference 2.1. Slip ring signals are:
• three (3) differential low voltage (<5 Volts dc) signals with returns and signal grounds,
• one (1) 10Base2 signal with its own shield,
• one (1) Giga-bit Ethernet, and
• one (1) 16-vdc power and return with Chassis Ground to 10 amps.
2. APPLICABLE DOCUMENTS
The following references are applied as stated in the following sections.
2.1. NAWC 80084397_A12M_REVC Slip Ring
2.2. MIL-STD-810G Test Method Standard for Environmental Engineering Considerations and Lab Tests
2.3. MIL-STD-461G, current revision, Electromagnetic Emission and Susceptibility Requirements for the Control of
Electromagnetic Interference.
2.4. NAVSEA Instruction 5100.3B, Mercury Exclusion
3. TECHNICAL DESIGN AND PERFORMANCE REQUIREMENTS
The Slip Ring is fabricated to the mechanical dimensions and with functional interfaces defined in NAVAIR drawing reference 2.1 and as shown in the sketch below.
GMPM2-B112PT-16K1-460M
M80 -4602605
DIRECT DIRECT
MNSO -09 -V4 -N-ETH MNSO -15 -V4-N-ETH
SLIP RING
DIRECT
MNSO -15 -V4-N-ETH
J48
J46 J47
P16 P56
P 4 3
5 / 9 UNCLASSIFIED
3.1 ELECTRO-MECHANICAL CONNECTORS
The slip ring has three connectors within the slip ring housing.
J46 & J48 CONNECTOR
J46 connects to J48 and transmits Gigabit Ethernet (802.3ab) signals. Both connectors are a fifteen (15) Nano-pin Omnetics MNSO-15-V4-N-ETH.
Signal Name FROM: SLIP RING TO: J46 Pin #
FROM: SLIP RING
TO: J48 Pin #
Current/Pairing requirements
CGND Shell Shell
GND 1 1 Ground ref., no current GND 2 2 Ground ref., no current Ethernet A+ 3 3
802.3ab Ethernet A- 4 4 GND 5 5 Ground ref., no current GND 6 6 Ground ref., no current Ethernet B+ 7 7
802.3ab Ethernet B- 8 8 Ethernet C+ 9 9
802.3ab Ethernet C- 10 10 GND 11 11 Ground ref., no current GND 12 12 Ground ref., no current Ethernet D+ 13 13
802.3ab Ethernet D- 14 14 GND 15 15 Ground ref., no current
J47 CONNECTOR
J47 is a nine (9) pin Omnetics MNSO-09-V4-N-ETH.
Signal Name FROM: SLIP RING TO: J47 Pin #
FROM: SLIP RING
TO: W18 P43
Current/Pairing requirements
CGND Shell Shell
- 1 -
DIFFa+ 2 19 100 Ohm Differential pair DIFFa- 3 20
DIFF-COM+ 4 25
50 Ohm Differential pair DIFF-COM- 5 26
DIFFb+ 6 21 100 Ohm Differential pair DIFFb- 7 22
DIFFc+ 8 23 100 Ohm Differential pair DIFFc- 9 24
MOUNTING
Connectors J46, J47, and J48 are mounted as vertically launched connectors.
CUTOUT
Reference 2.1 shows slip ring cover provides a cutout to access recessed J46, J47, or J48 connectors.
6 / 9 UNCLASSIFIED
GROUNDING
The connector shells are grounded to the Slip Ring chassis with < 5 milliohm resistance.
3.2 ELECTRO-MECHANICAL CABLES
Three cables, W15, W18, and W26 are direct cable leads emanating from the slip ring housing (soldered in place, emerging from the slip Ring housing with no connector at housing surface). Lengths of each cable are identified in reference 2.1.
W15 CABLE
W15 is a 16 AWG Twisted Shielded Pair cable which provides 16 VDC at P56, which is a GlenAir GMPM2-B112PT- 16K1-460M. Length is identified in reference 2.1. The Shield shall be carried from the shell of P56 using a backshell or other method and be connected to the slip ring case.
Signal Name FROM: W15 P56
TO: SLIP RING
FROM: SLIP RING
TO: W18 P43
Current/Pairing requirements
Shield Shell Shell Shield – no current
GND A 9,10,11,12 4 Ᾱ, 5 Ầ, 16 V, DC
16V_Main B 1,2,3,4 4 Ᾱ, 5 Ầ, 16 V, DC
Note: P56-A (GND) is rounded side of GlenAir GMPM2-B112PT-16K1-460M
W26 CABLE
W26 is a 16 AWG Twisted Shielded Pair cable which provides 16 VDC to P16, which is a GlenAir GMPM2-B112PT- 16K1-460M. Length is identified in reference 2.1. The Shield shall be carried from the shell of P16 using a backshell or other method and be connected to the slip ring case.
Signal Name FROM: W26 P16
FROM: SLIP RING
TO: W18 P43
Current/Pairing requirements
Shield Shell Shell Shield – no current
GND A 5,6,7,8 4 Ᾱ, 5 Ầ, 16 V, DC
16V_Main B 14,15,16,17 4 Ᾱ, 5 Ầ, 16 V, DC
Note: P16-A (GND) is rounded side of GlenAir GMPM2-B112PT-16K1-460M
7 / 9 UNCLASSIFIED
W18 CABLE
W18 is a shielded cable terminated at P43 and the Slip Ring. The cable consists of sixteen (16) 26 AWG wires which provide 16 Volts dc and GND to P56 and P16, a chassis ground (CGND), a Slip Ring GND, and four (4) 28 AWG Differential pair signals to J47. The cable has a Harwin M80-4602605 (connector number P43) on one end, and enters the Slip Ring directly through the other end. Length is indicated in reference 2.1.
Signal Name FROM: W18 P43
FROM: SLIP RING
TO: **
Remarks
Shield Shield - Connect Shield to Slip Ring Chassis
16V_MAIN
W15 P56-B
8 Ᾱ, 10 Ầ, 16 Vdc
W26 P16-B 15
GND
W15 P56-A
8 Ᾱ, 10 Ầ, 16 Vdc
W26 P16-A
18 GND
Connect to internal GND of the Slip Ring
CGND 13 Connect to Case
DIFFa+ 19 J47-2 0.01 Ᾱ, 0.1 Ầ, 1 V, 10 MHz DIFFa- 20 J47-3 0.01 Ᾱ, 0.1 Ầ, 1 V, 10 MHz DIFFb+ 21 J47-6 0.01 Ᾱ, 0.1 Ầ, 1 V, 10 MHz DIFFb- 22 J47-7 0.01 Ᾱ, 0.1 Ầ, 1 V, 10 MHz DIFFc+ 23 J47-8 0.01 Ᾱ, 0.1 Ầ, 1 V, 10 MHz DIFFc- 24 J47-9 0.01 Ᾱ, 0.1 Ầ, 1 V, 10 MHz
DIFF-COM+ 25 J47-4 0.1 Ᾱ, 0.1 Ầ, 5 V, 10 MHz DIFF-COM- 26 J47-5 0.1 Ᾱ, 0.1 Ầ, 5 V, 10 MHz
CABLE EXITS
Cables W15, W26, and W18 shall exit the slip ring housing 45o radially outward from the slip ring face as indicated in reference 2.1.
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3.3 ENVIRONMENTAL SPECIFICATIONS
Shelf Life The slip ring assembly shall have a shelf life of 30 years, wherein it will have been subjected to the storage environments defined below, as demonstrate by tests methods listed.
Storage Temperature Temperature of - 40 to +85 degrees Centigrade Ref 2.2, Methods 501.5 High Temperature and 502.5 Low Temperature Procedure I-storage constant temperature exposure (not cyclic exposure)
Storage Humidity Standard Ambient (Relative Humidity 20-80%), Ref 2.2, Method 507.5 tailored
Handling & Assembly During acceptance and/or assembly, the slip ring will be subject to the following environmental dynamic changes, without loss of functional performance after restored to operation environment.
Handling Shock Use Ref 2.2, Methods:
516.6 I (Functional – see table 516.IV, Step 4.62 Procedure I – Functional Shock) and
516.6 -VI (Packaged: per table 516.6-VI Transit Drop: drop from 48 in, on each face, edge, corner – total of 26 drops).
Pressure Transients Withstand a vacuum to 0.25 +0/-0.15 Torr for 24 hrs.
Withstand a single-event pressure increase from ambient at of 2.0 +0.5/−0 psig of R134a refrigerant with nitrogen added until the component internal pressure reaches a terminal pressure of 50.0 +5.0/-0 psia, then to withstand that terminal pressure for 30 minutes.
Operational Environment
MTBF
Once made operational, the slip ring assembly shall be designed to operate with signal continuity and signal isolation performance remaining within 95% of original acceptance measurements after 9,000 hours of operation at 1 Hz rotation rate and when subjected to the operational marine environments listed below and as will be proven using the analytical and test methods indicated and tailored.
Temperature -40 to +85 degrees Centigrade Ref 2.2, Methods 501.5 High Temperature and 502.5 Low Temperature Procedure II, constant temperature exposure (not cyclic exposure).
Pressure Enclosed in dry nitrogen or dry air atmospheric housing at 15.0 +5/-0 psig maintained.
Humidity Dew point less than -20oC Ref 2.2, 507.5 tailored.
Note: Nominal diurnal cycle: (1) Assembly is OFF (No adjacent thermal load) & thermally saturated at -4oC; (2) Enter ambient Temp of -40oC; (3) Soak temp cools to -20oC;
(4) condensation accumulates until unit is turned on to operate, which coincides with internal thermal loads to raise internal ambient temp above -20oC. Ref 2.2, 520.4, tailored
Vibration Ref 2.5, Up to 28 Hz vibration.
Ref 2.2, Method 514.6 Vibration or 520.3 Temperature, Humidity, Vibration and Altitude, 9 / 9 UNCLASSIFIED
3.4 EMI
The slip ring assembly shall perform in accordance with the Electro Magnetic Interference (EMI) standard defined in reference 2.3.
(1) Perform RE101 in accordance to Reference 2.3.
(2) Perform CS114 in accordance to Reference 2.3.
3.5 SIGNAL CONTINUITY
While rotating at 60 RPM, the End-to-End signal continuity of each input to its respective output(s) shall achieve an average resistance which remains less than 20 milliohms when captured for a 10 second duration measurement.
3.6 SIGNAL ISOLATION
While rotating at 60 RPM, Pin-to-Pin average isolation resistance of each connector remains greater than 10 Mega Ohms when captured for a 1-minute duration measurement. All low voltage (≤5 V) connector pins and cable wires require 20 dB crosstalk isolation.
To verify signal line to other signal lines are isolated at signal voltage and signal frequency, perform the following:
Using a signal generator, transmit an input 100 Mhz signal at-1 Volts dc to +1 Volts dc down each signal line and using an oscilloscope measure the observed signal level on both ends of all other signal lines. Observed Signal on other signal lines shall be 20 dB lower than signal line being transmitted on.
3.7 IMPEDANCE
While conducting EMI tests in 3.4, measure and record the impedance of each signal line.
3.8 16 VDC POWER CONTINUITY
While rotating at 60 RPM and unpowered, the continuity of the 16 Volts dc power line End-to-End (input to its two outputs) shall achieve an average resistance which remains less than 20 Milli Ohms when captured for a 10 second duration measurement.
When rotating at 60 RPM and powered with a 20-watt load on W26 and a 40-watt load on W15, the average voltage drop of 16 Volts dc power line (voltage at input to its respective outputs) remains less than 100 millivolts when captured for a 10 second duration measurement.
3.9 16 VDC POWER ISOLATION
While rotating at 60 RPM and unpowered, Pin-to-Pin isolation (insulation) resistance of each connector remains greater than 10 Mega Ohms when captured for a 1-minute duration measurement.
While rotating at 60 RPM and powered, Power Line Pin-to-Signal Line Pin voltage of each connector remains less than 100 millivolts when captured for a 1-minute duration measurement.
3.8 MECHANICAL SPECIFICATIONS
The slip ring assembly shall meet the mechanical constraints defined by Reference 2.1 and as indicated below.
10 / 9 UNCLASSIFIED
Operating Speeds Nominal 60 RPM constant speed operation will be in the forward direction (clockwise, looking down onto rotor - sheet 1, reference 2.1).
Internal Bearing One bearing lubricated as defined below Bearing Lubrication Low temperature grease in accordance with Mil-G-23827C and selected for long periods of non-rotation (ie minimize grease migration).
Oscillatory Motion: None Torque Starting and running torque are to be less than 1500 gm-cm
3.9 MARKINGS
The slip ring assembly housing, cable wire numbers, (and connectors on production units) shall be marked with the wiring nomenclature shown on the referenced NAWC interface drawing using an abrasion resistant black ink or other indelible marking. The slip ring assembly part number and serial number shall be marked in a similar way.
3.10 MERCURY EXCLUSION
The supplies furnished under this contract shall not contain functional mercury in accordance with Ref 2.4. Functional mercury is that mercury or mercury compound required for proper operation of the supplies or without the presence of which the supplies would fail to function properly. External contamination by metallic mercury or mercury compounds shall be cause for rejection of the supplies. The mercury vapor concentration in trapped air about any tested item(s) shall not exceed 0.01 mg per cubic meter.
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