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FBO DAILY - FEDBIZOPPS ISSUE OF SEPTEMBER 03, 2016 FBO #5398
DOCUMENT

59 -- GPS Clock Equipment - Attachment

Notice Date

9/1/2016
 

Notice Type

Attachment
 

NAICS

334515 — Instrument Manufacturing for Measuring and Testing Electricity and Electrical Signals
 

Contracting Office

FEDERAL AVIATION ADMINISTRATION, AAQ510 EN - Eastern Service Area (Atlanta, GA)
 

Solicitation Number

25378
 

Response Due

9/28/2016
 

Archive Date

9/28/2016
 

Point of Contact

Kimberly Burt, kimberly.burt@faa.gov, Phone: 404-305-5016
 

E-Mail Address

Click here to email Kimberly Burt
(kimberly.burt@faa.gov)
 

Small Business Set-Aside

N/A
 

Description

Market Survey Purpose: This Market Survey is issued in accordance with Federal Aviation Administration (FAA) Acquisition Management System (AMS) Section 3.2.1.2.1. The purpose of this Market Survey is for the FAA to gain an understanding of the industry and to identify large and small businesses, equal or better test equipment to what we currently use/require to maintain our systems. Background: AJW-142, NAS Defense Programs, NDP Air Route Radar Systems, has a project with specialized needs in a GPS clock required for testing radar data time accuarcies referenced to the boresight of the radar antenna. The GPS Clock Equipment described in this document is the minimum requirement to test the time accuracies in the radar data messages. A subset of these requirements will be evaluated to determine the minimum set of requirements for a GPS clock source at all Common Air Route Surveillance Radars (CARSR) and Air Route Surveillance Radars Model 4 (ARSR-4) facilities based on the test results from initial time data accuracy testing. This GPS clock source will be installed at all CARSR and ARSR-4 facilities to meet the minimum requirements of radar data time accuracies as a requirement by the Surveillance Interface Modernization program. The GPS clock system provided by the vendor will be described in Figure 1. The vendor will provide information on a GPS Antenna, Lightning Protection Assembly, and GPS Receiver. The FAA will design the interconnecting cabling, GPS antenna mount, and the ground plane based on the Lightning protection assembly. If cabling other than LMR-400 is required, cable specification will need to be disclosed in response to this request. Figure 1: GPS Clock System Diagram The GPS Receiver will require industry standard outputs and a new developmental output format. The GPS Receiver will need to be modular in design. The GPS Receiver will also need to be upgradable to a Secure Selective Availability Anti-Spoofing Module (SAASM) compliant per CJCSI 6130.01C Enclosure E with a clear path to M-Code, but will not be required in these units. Initial purchase quantity would be four units. Units would include items 1 through 3. System Requirement: Upgradeability 1.Must be upgradeable into an SAASM configuration, provide detail how configuration would change to achieve SAASM configuration. Item 1, GPS Antenna Requirements Mechanical Requirements 1.Mounting hole information must be provided in response to this document 2.Connection to antenna will be a N-Type Female connector 3.Must be protected from environment and suitable for outdoor installation, define protection in response to this document 4.Temperature Range: -40 ° to 85 ° C Performance Requirements 1.Must be capable of driving the GPS L1 and L2 frequency 375 feet with LMR-400 or equivalent cable. 2.Frequency Range: L1: 1575.42 ± 15 MHz and L2: 1227.60 ± 15 MHz Item 2, Lighting Protection Requirements Mechanical Requirements 1.Mounting hole information must be provided in response to this document 2.Input connection will be a N-Type Female connector and be clearly marked as input 3.Output connection will be a N-Type Female connector and be clearly marked as output 4.Temperature Range: -40 ° to 85 ° C Performance Requirements 1.Must protect GPS receiver from high energy discharges, clamping voltage must be matched to the GPS receiver maximum input voltage. 2.Minimum VSWR: 1.1:1 3.Maximum Insertion Loss: 0.1 dB Item 3, GPS Receiver Mechanical Requirements 1.Size: 19 ť rack mountable with mounting hardware, 1U height. Maximum depth 15 ť 2.Weight: <15 lbs 3.Input connector from antenna: Type N female 4.Operating Temperature Range: -20 ° to +55 ° C per MIL-STD-810F 501.4 5.Storage Temperature Range: -40 ° to +85 ° C per MIL-STD-810F 502.4 6.Humidity: 0% - 95% RH non-condensing @ 40 ° per MIL-STD-810F 507.4 7.Operating Altitude: 13,000 ft per MIL-STD-810F 500.4 8.Storage Altitude: 45,000 ft per MIL-STD-810F 500.4 9.Operating Shock: 5g, 11ms half sine wave per MIL-STD-810F 516.5 10.Storage Shock: 40g, 11ms half sine wave per MIL-STD-810F 516.5 11.Operating Vibration: 10-55Hz/0.07g2/Hz, 55-500Hz/1.0g2/Hz per MIL-STD-810F 514.5 12.Storage Vibration: 10-55Hz/0.15g2/Hz, 55-500Hz/2.0g2/Hz per MIL-STD-810F 514.5 Power Requirements 1.Power Source: 120 VAC, 60 Hz 2.Power Draw: Nominal 50W; Peak Maximum of 80 Watts Basic Requirements to Receiver 1.Synchronization Time from cold startup: <15 minutes 2.Synchronization Time from warm start: <5 minutes 3.Configuration Port: RJ-45, 10/100-base T 4.Visual Indications Front Panel: Power, GPS Lock, Fault, and GPS Time/Date Network Services 1.NTP Version 4, conforms with RFC1305 and supports NTP over AnycastManagement 2.IPv4/IPv6: Dual Stack 3.Syslog: Logging Communications 1.HTTP: Browser based configuration and monitoring 2.FTP Server: Access to files Security 3.Enable/Block Protocols 4.Password Protected 5.Standard encryption/authentication protocols 6.SSL Web-based Interface: SSL is used to secure HTTPS protocols to access configuration and status web pages 7.SSH: SSL and data compression 8.SCP 9.SFTP: FTP replacement operates over an encrypted SSH transport 10.SNMP v3: remotely configure and manage over an encrypted connection Output 1, 10MHz Frequency Output Requirements 1.Minimum of 1 output 2.Minimum output power: +10 dBm into 50 ohm, BNC 3.Accuracy (over 24 hours): 1x10-12 4.Medium Term Stability (Aging): 5x10-11 per month 5.Short Term Stability (Allan variance) @ 1 sec: 2x10-11 6.Short Term Stability (Allan variance) @ 10 sec: 2x10-12 7.Short Term Stability (Allan variance) @ 100 sec: 2x10-12 8.Temperature Stability: 1x10-10 9.Phase Noise @ 1 Hz: -80 dBc/Hz 10.Phase Noise @ 10 Hz: -98 dBc/Hz 11.Phase Noise @ 100 Hz: -120 dBc/Hz 12.Phase Noise @ 1 kHz: -140 dBc/Hz 13.Phase Noise @ 10 kHz: -140 dBc/Hz Output 2, PPS Output 1.Minimum of 1 output 2.Output connector: Female BNC 3.Output waveform: TTL (5v Peak to Peak), into 50 ohm, BNC 4.Accuracy to UTC: ±25 nanoseconds 5.Holdover Accuracy After 4 hours (constant temperature after 2 weeks of GPS lock): 0.25 µsecond 6.Holder Accuracy After 24 hours (constant temperature after 2 weeks of GPS lock): 1.5 µsecond 7.Holder Accuracy 30 days, at constant 70 ° F: 1 millisecond 8.Holder Accuracy 30 days, at constant 80 ° F: 1 millisecond 9.Holder Accuracy 30 days, at temperature variation from 70 ° F to 80 ° F: =2 millisecond Output 3, 1 Gbyte Precision Time Protocol 1.Minimum of 1 output 2.Output connector: 1 GB SFP 3.IEEE 1588-2008, PTPv2 compliant 4.Minimum Time Resolution: ±4 nanoseconds packet time stamping 5.Holder Accuracy 30 days, at constant 70 ° F: 1 millisecond 6.Holder Accuracy 30 days, at constant 80 ° F: 1 millisecond 7.Holder Accuracy 30 days, at temperature variation from 70 ° F to 80 ° F: =2 millisecond Output 4, IRIG 1.Minimum of 1 output 2.Output connector: Terminal Block 3.Output Protocol: IRIG-B 4.Signal Type: RS-485 Output 5, ASCII Time Code 1.Minimum of 1 output 2.Output Protocol: ASCII Time Code 3.Output connector: DB9 4.Signal Type: RS-232 Output 6, Pulse Input Time Stamping: This output would consist of two Ethernet outputs with configurable IP addresses. The module would accept incoming positional pulse data from two sources on one DB15 connector. The positional pulse data would consist of 16384 positional pulses and one north mark reference. The module would then output a timestamp for each of the 16384 positional pulses. The output would consist of a pulse counter value with an associated UTC timestamp. The pulse counter value would be reset to pulse 0 at the channel north mark reference. The module would be configurable to output the messages in blocks consisting of either 256 or 512 values. 1.Input: a.Connector: DB15 Male b.Signal Type: Differential RS-422 c.Signals Definition: Positional Pulse: improved Azimuth Change Pulse (iACP) North Mark Reference: Azimuth Reference Pulse (ARP) Ground: GND d.Pin Definintions: Pin 2 “ iACPA+ Pin 9 “ iACPA- Pin 8 “ GNDA Pin 4 “ ARPA+ Pin 11 “ ARPA- Pin 3 “ iACPB+ Pin 10 “ iACPB- Pin 15 “ GNDB Pin 5 “ ARPB+ Pin 12 “ ARPB- 2.Output connector: RJ-45 3.Accuracy: ±30 useconds per pulse 4.Output Protocol: To be provided with proposal, Pulse ID Counter and UTC Timestamp Submittal Information: The FAA is soliciting industry for those companies with a proven capability to provide us GPS time source described above. Electronic submittal documents provided by capable vendors should be in portable document file (PDF) or Microsoft word format. Submissions should not exceed 10 pages in length. Vendors must submit the following: Provide a description of the GPS receiver and its outputs to prove it is equal or better and compatible with existing units Identify which items are standard products and which items will be developmental. On the developmental outputs, define an expected design time period. Provide a completed Business Declaration Form No solicitation exists; therefore, do not request a copy of the solicitation. The FAA is not seeking unsolicited proposals at this time. This Market Survey must not be construed as either a promise to award a contract or an obligation for the Government to provide compensation for information associated with the preparation and submittal of inquiries addressing this Market Survey. The FAA reserves the right to reject, in whole or in part, any private sector input as a result of this market survey. Responses will not be returned. Respondents will not be notified of the results of this survey. If you're viewing this announcement from a source other than Federal Aviation Administration Contract Opportunities (FAACO), visit https://faaco.faa.gov/index.cfm/announcement/view/25378 to view the original announcement.
 

Web Link

FBO.gov Permalink
(https://www.fbo.gov/spg/DOT/FAA/SR/25378/listing.html)
 

Document(s)

Attachment
 

File Name: FAA Market Survey GPS clocks DRAFT 2016-08-24 version 2 (doc) (https://faaco.faa.gov/index.cfm/attachment/download/69174)

Link: https://faaco.faa.gov/index.cfm/attachment/download/69174

 

Note: If links are broken, refer to Point of Contact above or contact the FBO Help Desk at 877-472-3779.
 

Record

SN04252704-W 20160903/160902000325-4a5186fa49f5277e2917e3b56663792e (fbodaily.com)
 

Source

FedBizOpps Link to This Notice
(may not be valid after Archive Date)

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