NanoSync IV® Model 424 -Low Profile
The NanoSync IV Low Profile is a smaller form factor GPS Position, Navigation, Time (PNT) and Frequency reference system that provides multiple reference outputs includes support for NTP & PTPv2 IEEE 1588-2008. The NanoSync IV Low Profile has a OCXO oscillator and is available with a civilian C/A GPS receiver or a SAASM/M-Code GPS receiver for military users. The NanoSync IV is packaged in a small, rugged enclosure ideally suited for embedded electronic warfare applications.
The NanoSync IV – Low Profile has been demonstrated to be compliant to the Joint Airborne SIGINT Architecture (JASA) Version 3.0, Annex 1, for Time, Frequency, Navigation and Geodesy (TFNG), making it suitable for Electronic Warfare (EW) COMINT and ELINT applications in fixed site, airborne and shipboard environments.
- Description
- Output Specs
- GPS Receiver Options
- Input/Output
- Power Options
- Chassis Dimensions
- Environmental
- Notes
Description
PRODUCT DESCRIPTION
The NanoSync IV Low Profile is a smaller form factor GPS Position, Navigation, Time (PNT) and Frequency reference system that provides multiple reference outputs includes support for NTP & PTPv2 IEEE 1588-2008. The NanoSync IV Low Profile has a OCXO oscillator and is available with a civilian C/A GPS receiver or a SAASM/M-Code GPS receiver for military users. The NanoSync IV is packaged in a small, rugged enclosure ideally suited for embedded electronic warfare applications.
The NanoSync IV has been demonstrated to be compliant to the Joint Airborne SIGINT Architecture (JASA) Version 3.0, Annex 1, for Time, Frequency, Navigation and Geodesy (TFNG), making it suitable for Electronic Warfare (EW) COMINT and ELINT applications in fixed site, airborne and shipboard environments.
NanoSync IV incorporates proven features designed into all FEI-Zyfer products, including exceptional holdover performance when GPS signals are lost or degraded. This assures continued system operation as a time and frequency reference. The NanoSync IV can be monitored and controlled through an RS-232 port using FEI-Zyfer’s Serial Communication Protocol and via the 10/100Base-TX RJ-45 Ethernet port.
As with all FEI-Zyfer time and frequency products, the NanoSync IV incorporates advanced, proprietary learning algorithms that compensate for external temperature changes and aging characteristics of the oscillator while operating in holdover. This FEI-Zyfer feature ensures accuracy and consistent performance throughout the specified operating temperature range.
SYSTEM FEATURES
- High Performance Position
& Navigation Engine - Precise Time & Frequency
Reference - COTS for Military
Applications - Compact, Rugged Design
- Low Power – Less than
20W Steady-State - Wide Operating Temperature Range
- JASA V3 Annex 1
TFNG Compliant - No Maintenance Required
10 MHz Output: | |
Waveform: | Sine wave, AC coupled |
Connector: | (2) SMA Female |
Amplitude: | 13 dBm +3/-1 into 50 Ω |
Harmonic Distortion: | ≤ -50 dBc(f). |
Non-Harmonic Distortion: | ≤ -60 dBc |
Frequency Accuracy: | |
Locked to GPS: | ≤ 1E-12 (24 hour average) |
Holdover (with FE-5680B Rb) (a): | ≤ 7.5E-11 at 24 hours with ± 10° C temperature change. |
Short Term Stability (Allan Deviation, typical): | |
1 Second: | ≤ 3E-11 |
10 Seconds: | ≤ 1E-11 |
100 Second: | ≤ 3E-12 |
Harmonics: | -40 dBc |
Spurious Level: | -70 dBc |
Phase Noise | |
1 Hz: | -80 < dBc/Hz |
10 Hz: | -100 < dBc/Hz |
100 Hz: | -105 < dBc/Hz |
1 kHz to 100 kHz: | -115 < dBc/Hz |
1 PPS Output (Pulse, Rising Edge on-time) (b): | |
Connector: | (2) SMA Female |
Drive Level: | TTL into 50 Ω |
Pulse Width: | 2 ms w/ ≤ 20 ns Rise Time |
Synchronization: | Rising edge on-time |
1PPS Jitter: | ≤ ± 5 ns 2σ (95 %) |
1 PPS Time Accuracy: | |
Locked to GPS: | < 25 ns 2σ (95 %) to UTC |
Holdover (with FE-5680B Rb) (a): | ≤ 4.3 µs @ 24 hours after 48 hours locked operation |
Time Code Output Options (User Programmable): | |
Connector: | (1) SMA Female |
BCD: | 24b or 40b |
HaveQuick: | HaveQuick 2(STANAG 4246) PTTI HaveQuick (ICD-GPS-060) Extended HaveQuick (STANAG 4430) |
IRIG: | B02x (x=2,3,6,7) |
Trimble Force 22E (MRU) GRAM SAASM/M-Code GPS Receiver For Use in Man-Portable through High Dynamic Environments: |
|
Velocity (High Dynamic Limit): |
Up to ± 400 meters/second |
Acceleration (High Dynamic Limit): | Up to ± 40 meters/second2 |
Jerk (High Dynamic Limit): | Up to ± 4 meters/second3 |
All-in-view 24 Channel Receiver, with continuous independent tracking: | |
Simultaneous L1 (C/A, P(Y)) and L2 (P(Y)) Dual Frequency Tracking |
|
Receiver Interface Protocols: | ICD-TNL-153C, ICD-TNL-167 SHCI, NMEA 0183 v3.2 |
Time Accuracy: | |
UTC(USNO): | ≤ 100 ns 1σ (68.3 %) |
GPS Time: | ≤ 40 ns 2σ (95.5 %) |
Acquisition Time / TTFF: | |
Hot Start: | ≤ 10 seconds |
Warm Start: | ≤ 60 seconds |
Position & Velocity Accuracy (in State 5, L1 & L2, WAGE enabled & within operating parameters: | |
SDGPS: | ≤ 2 meters CEP |
WAGE: | ≤ 4 meters CEP |
Velocity (High Dynamic Environment): | 0.1 meters/second (RMS) |
Rockwell Collins MPE-S GB-GRAM SAASM/M-Code GPS Receiver For Use in Man-Portable, Surface Vehicle or Low Dynamic Environments: | |
Acceleration (Surface Vehicle Limit): | Up to ± 3 meters/second2 |
Jerk (Surface Vehicle Limit): | Up to ± 2 meters/second3 |
All-in-view 12 Channel Receiver, with continuous independent tracking: | |
Simultaneous L1 (C/A, P(Y)) and L2 (P(Y)) Dual Frequency Tracking |
|
Receiver Interface Protocols: | ICD-TNL-153C, NMEA 0183 v3.2 |
RAM/FLASH and FLASH/FLASH versions of the MPE-S available and supported | |
Time Accuracy: | |
UTC(USNO): | ≤ 200 ns 2σ (95.5 %) |
GPS Time: | ≤ 52 ns 2σ (95.5 %) |
Acquisition Time / TTFF: | |
Hot Start: | ≤ 10 seconds |
Warm Start: | ≤ 90 seconds |
Position & Velocity Accuracy (in State 5, L1 & L2, WAGE enabled & within operating parameters: | |
SDGPS: | ≤ 2 meters CEP |
WAGE: | ≤ 4 meters CEP |
Velocity (Surface Vehicle): | Better than 4.0 meters/second (3D, 2σ) |
GPS Antenna Interface: | |
Power: | 5 VDC @ 100 mA |
Connector Type: | SMA Female |
Input Gain Required: | + 10 dB |
Standard Input: | +24 VDC (18 V to 28 VDC, externally regulated) |
Warm-Up: | 40 W maximum @ 25 °C |
Warm-Up Time: | ≤ 10 minutes |
Steady State: | 20 W maximum @ 25 °C |
Isolation: | None, input return connected to chassis/signal ground |
Optional: 704A / 1275 D Compliant | +15 VDC to +33 VDC |
Warm-Up: | 50 W maximum @ 25 °C |
Warm-Up Time: | ≤ 10 minutes |
Steady State: | 30 W maximum @ 25 °C |
Height: | 89 mm (3.50″, side-mount) |
Width: | 102 mm (4.02″ excluding I/O connectors) |
Depth: | 211 mm (8.27″ excluding LED’s and/or SAASM/M-Code connectors) |
Weight: | < 2.2 kg (4.9 lbs.) |
Operating Temperature: | -20 °C to 50 °C (@ baseplate) |
Temperature Rate of Change: | 10 °C/Hour maximum |
Storage Temperature: | -40 °C to +100 °C |
Relative Humidity: | 5 % to 95 %, non-condensing |
Altitude, Operating: | 0 to 35000 feet |
Altitude, Storage: | 0 to 40000 feet |
(a) After 48 hours of GPS locked operation, fixed antenna location and antenna delays entered.
(b) 1 PPS output can be disabled until GPS lock is achieved and time offset error is less than a user programmable amount.
(c) U.S. Government policy restricts the sale of Precise Positioning Service (PPS) equipment to those
authorized by the U.S. Department of Defense. Non-U.S. authorized users must purchase PPS equipment
through the Foreign Military Sales (FMS) process.