Attachment B - Bid Sheet.docx

Attachment B-Bid Sheet-RFB 758 2500000479-KSP Tactical Airborne System Cessna 182

ATTACHMENT B – BID SHEET

RFB 758 2500000479 – KSP Tactical Airborne System for Cessna 182

ENTER PRICE, DELIVERY AND WARRANTY ONLY, IN THE FIELDS PROVIDED BELOW.

ANY MODIFICATIONS TO THIS FORM MAY RESULT IN REJECTION OF BID OFFER.

DO NOT ATTACH A SEPARATE QUOTE.

BIDDER NAME:

Line #1 - Camera System

Provide a MX-10 camera system for a Cessna 182 airplane that provides both day, thermal imaging, and low light capability with the specifications below. No substitutions permitted.

Gyro-Stabilized EO/IR Imaging System

Sensor Payload Configuration:

· High-Definition Infrared Imager

· 1280 x 720p

· Cooled InSb 3-5 micron Mid-Wave IR

· 8 micron pixel pitch maximum

· Continuous zoom

· Minimum narrow HFOV of 2.8°

· 2X and 4X Digital Zoom

· High-Definition Electro Optical Imager

· 1920 x 1080 CMOS high sensitivity Daylight Sensor

· Continuous Zoom

· Minimum Narrow HFOV of 1.2°

· 2X and 4X Digital Zoom

· High-Definition Electro Optical Spotter Imager

· 1920 x 1080 CMOS high sensitivity Daylight Sensor

· Fixed Focal Length (for improved image resolution)

· Minimum Narrow HFOV of 0.61°

· 2X and 4X Digital Zoom

· Low Light Imager

· 1092 X 614 pixel dual channel with daylight imager

· Monochromatic, near IR sensitivity

· Wide angle zoom optic

· Laser Illuminator Narrow Divergence and Laser Range Finder

· Integrated missile grade IMU mounted on the optical bench to support both gimbal stability and geo-pointing (co-located with imaging sensors)

· Embedded GPS processor

· Enhanced Image Processing for all sensors (Local Area Contrast Enhancement, Digital Contrast Enhancement, Edge Sharpening, Image Noise Reduction)

· System configurable for either 720p or 1080p by end-user

· Pseudo-Color HDIR Capability

· Picture-In-Picture (PiP)

· Image Fusion

· Remote Control Subsystem (RCS) Interface

· Three HD video output streams and two SD video streams

Gimbal Specification:

· Four Axis active stabilization

· 2-axis inner (pitch/yaw) and 2-axis outer (azimuth/elevation)

· 6-axis passive vibration isolation (pitch/roll/yaw)

· 10 micro-radian or less typical stability on all sensors without the use of:

· External vibration isolators located outside of the payload assembly

· Wire-rope stye isolators exposed to external environmental conditions

· Fast steering mirrors or other electronic image stabilization methods

· Stability performance must be verifiable in flight by system operator

· Geo-Pointing capability

· ≤2.5mrad or better pointing accuracy typical without the use of a laser range finder

· 11” max turret dia. (excluding connector interface)

· 14.0” max turret height (excluding mounting interface)

· 38 lbs max turret weight (excluding mounting interface)

· Elevation Coverage: +90⁰ to -120⁰

· Azimuth Coverage: 360⁰ continuous

System Integration Requirements:

· Interchangeable with existing EO/IR imaging system

· Fully interoperable with existing aircraft wiring and integrated mission equipment without the use of third-party adaptor cables

· Fully integrated/compatible with the Shotover/Churchill ARS, AeroComputers UC-6000, CartNav AIMS and Force X mapping systems

· Available Interfaces RS-422, RS-232, Mil-Std-1553B and Ethernet

· Power requirements 28VDC, 112 w (280 W max), 4 amp steady state (10 amp max)

User Interface:

· Ruggedized Hand Controller with integrated backlighting

· Maximum 2.2Lbs and 4.25’ (W) x 9” (L) x 3” (D)

· Laser Arming Panel

Support:

· Field Support technicians for on-site service support

· Multiple (minimum of 3) North American support/repair centers

Line #2 Mapping System:

Provide a Churchill Mapping system that interfaces with a Wescam MX 10 camera system that provides an augmented reality system (ARS-750 ATOM 2 and connection Kit) for a Cessna 182 Airplane with the specifications listed below. No substitutions permitted.

Augmented Reality System (ARS-750 ATOM 2 and Connection Kit):

Removable Media Slots USB 3.0 (x2) USB 2.0 (x1) Front Connections USB 3.0 (x2) USB 2.0 (x1) SO21 1JW Rear Connections SDI Out #1 (mirrored x2) - up to 4K60 SDI Out #2 (x1) - up to 1080p30 SDI Input (x2) - up to 1080p60 RS-422 (x1) RS-232 (x3) Audio In (x2)/Out USB 2.0 PS2 Keyboard (x1) PS2 Mouse (x1) Gigabit Ethernet

· Specification Characteristic Product Designation/Description SHOTOVER Systems GEAR-750 / ARS-750 with ATOM 2 Mission Computer

· Physical Dimensions 7.25” L x 5.75” W x 1.875” H (184.2 mm x 146.1 mm x 47.6 mm)

· Weight 2.75 Lbs. (1.25 Kg) with +/- .05 LBS [0.02 kg]

· Environmental Qualifications DO-160 Qualified

· Operating Temperature Range-20°C to +70°C

· Maximum Operating Altitude +45,000 feet [+13,716m]

· Input Voltage 28VDC (normal operating range: 18 - 30VDC)

· Input Current 2.3A on 28VDC

· Power Consumption Average Power Draw is 59 WATTS (2.1A ON 28VDC) Maximum Power Draw is 95 WATTS (3.4A ON 28VDC)

· Circuit Breaker Requirement Recommended 5.0A rated

· Connection Types

· Protocols, and Standards

· LEMO (1x) J1 – Power

· LEMO (1x) J2 Ethernet

· LEMO (1x) J4 – Serial COM port

· BNC (1x) J5 – BNC HD-SDI (secondary video out)

· BNC J6, J7 – HD-SDI 1 & HD-SDI 2 (video in)

· BNC J8, J9 – HD-SDI 1 & HD-SDI 2 (video out)

· Video-in Support SDI Input (x2) - up to 1080p (60 fps)

· Video-out Support SDI Out #1 (mirrored x2) - up to 4K (60 fps) SDI Out #2 (x1) - up to 1080p (30 fps)

· Video-out Supported Resolutions

· 720p (50 fps) | 720p (60 fps) | 1080p (25 fps)

· 1080p (30 fps) |1080i (50 fps) | 1080i (60 fps) | 1080p (60 fps)

· 4k (60 fps) | 20p (59.94 fps) |1080p (29.97 fps) | 1080p (59.94 fps)

· 1080i (59.94 fps) | 4K (25 fps) | 4K (30 fps)

· Metadata Standard KLV MISB/STANAG 4609 compliant

· Video Codecs H.264 (MPEG-4 AVC) H.262 (MPEG-2)

POWER CABLE:

· The connection to 28V input on the ATOM 2 and 28V GND are highly recommended per manufacture’s specifications to be spirally laid. 75-ohm HD-SDI COAX Cable Option A PicWire V78209 is highly recommended per manufacture’s specifications for 3G-SDI and higher data rate signals (6G-SDI, 12G-SDI). The proper connector is PicWire P/N 190712. Option B RG59 is also recommended per manufacture’s specifications for 3G-SDI and higher data rate signals (6G-SDI, 12G-SDI). The proper connector is Amphenol Connex P/N 112123. Option C If RG179 is required by other equipment (ex. MX-10 gimbal), then for EMI purposes, DOUBLE high performance 360-degree EMC individual braid shielding360-degreeone to RG179 cable from end to end. The proper connector is Amphenol Connex P/N 112133.

USB CABLE:

· USB 2.0 cabling is sufficient for all ATOM 2 functions. USB performance cannot be guaranteed at cable lengths greater than 6ft without the use of an extender.

ETHERNET CABLE:

· Picwire PIC E50824 is highly recommended. EMTEQ D100-0824-006 is also highly recommended.

ALL OTHER CABLES:

· MUST BE SHIELDED. All other cable can be selected by installer and all cables must be shielded, including power cables.

Line #3 - Display Screen and Controller:

Macro-Blue Display:

Provide a Macro Blue Display in Rear Seat area of Cessna 182. Including a movable mount style device for screen and controller. Screen Specifications listed below. No substitutions permitted.

· P/N: MB12W-N33040B00

· Q-Series Standard Display, 12.1", 16:10 Aspect Ratio, Landscape

· NVIS, Dual-Mode (NVIS/DAY), Meets MIL-STD 3009

· PCAP Touchscreen, Works with Gloves and Bare Fingers

· Built-In Dual-Knob Controls

· (4) 3G HD-SDI Video Inputs

· 1280 x 800 WXGA, 1500 NITS, Meets MIL-L8562A for Sunlight Readability and Contrast Ratio

· DO-160G Qualified

· Includes Patented Dual Host Touch Technology

· Instant Switching Between Signal Sources with Exclusive Signal Lock™ Technology

· Multiple Layouts (7): Single, Split Screen, Quad-View, C-Layout, E-Layout, PIP, PAP

· Includes Leader-Follower Display App

· USB Progaming & Service Port

· 3-Year Warranty - Parts & Labor

· 651-014REVA00 P/N: 651-014REVA00

· Install Kit J1 (Power and Comm) Q-Series

· (1) 528-001-16M11-19SA Circular Connector, HTS: 8536.69.4020, SCH-B: 8536.69.4000 COO

· (1) 528-809S060-3 Boot Shrink, HTS: 8538.90.8180, SCH-B: 8538.90.0000 COO

· P/N: 651-023

· Service Port (BULGIN), Q-Series

· BULGIN P/N: PX0844/B/0M50/B

· BULGIN P/N: PX0711

Line #4 - Installation Tactical Airborne System Cessna 182

Technisonic TDFM-9100 All-Band Airborne Radio and Audio Panel:

· The TDFM-9100 All-Band Airborne Radio is currently owned by the Commonwealth and will need the following:

· TDFM 9100 All-Band Airborne Radio - Installation only quote

· Audio panel will need to be provided by installer along with installation quote

· Model: TDFM-9100 w/Type A Digital Module

· TiL Part No. 121270-2-91-AZZ-P91655

· Jupiter Avionics Corporation Dual Audio control Audio panel

· Model #JA94-001A

· 28 VDC

· 1.99LBS

Installation:

· Must install Churchill mapping system, MX-10 camera, and Macro Blue Monitor system per manufacturer specifications. The installer provides monitor system and camera controlling device.

· Remote Mount Military-Style Rotary Knob Controller and keyboard

· Must install TDFM-9100 Radio provided by customer and Audio Panel compatible with KSP Radio Channels (Compatible Audio Panel Needs to be purchased by installer).

· Rear Seat installation with movable type mounting device for screen and controller and keyboard

· Installer must have personnel on site that have completed at least 3 previous completion installs and show proof. Provide names, addresses, contact numbers and/or emails.

· Installer must provide proof of FAA Authorized Repair Station. Provide Certificate.

· Install center must be located within 250 miles of Frankfort KY.

· Installer must complete an actual weight and balance once aircraft is complete.

· Installer must complete the installation within 90 days once work has started.

· Installer must start work within 30 days of receiving all equipment.

TOTAL DELIVERED COST:

DELIVERY TIME (# DAYS AFTER RECEIPT OF ORDER):

WARRANTY TERM (# MONTHS):

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