(English) IT-ISS FLY-981
(English)
The iNetVu® FLY-981 Flyaway Antenna is a 98 cm satellite antenna system which is a highly portable, self-pointing, auto-acquire unit that is confgurable with the iNetVu® 7710 Controller providing fast satellite acquisition within minutes, anytime anywhere. It can be assembled in 10 minutes by one person.
Field Upgradable to FLY-98G, FLY-98V or FLY-98H
Intellisystem Technologies thanks to its strong partnership with C-Com Satellite Systems Inc. is not only their official systems distributors but also a system integrators with added value support and OEM enginering able to work on custom customer’s Industrial and Research & Development projects.
If you operate in Ku-band, the FLY-981system is easily configured to provide instant access to satellite communications for any application that requires reliable and/or remote connectivity in a rugged environment. This next generation Flyaway Ku terminal delivers afordable broadband Internet services (High-speed access, Video & Voice over IP, file transfer, e-mail or web browsing). Ideally suited for industries such as Oil & Gas Exploration, Military Communications, Disaster Management, SNG, Emergency Communications Backup, Cellular Backhaul and many others.
Descrizione
The Intellisystem Technologies Integrated Satellite Solutions (IT-ISS) provides two-way broadband satellite connectivity for non-terrestrial WAN Backup, IP multicast, and broadband internet access.
Features
• One-Piece high surface accuracy, offset feed, steel reflector
• Heavy duty feed arm capable of supporting up to 5kg (10lbs) RF Electronics (LNB & BUC)
• Designed to work with the iNetVu® 7710 Controller
• Works seamlessly with the world’s most popular commercially available Ku modems
• Axis motorization
• Supports manual control when required
• One button, auto-pointing controller acquires Ku-band satellite within 2 minutes
• Captive hardware / Fasteners
• 10 minute assembly by one person, no tools required
• Compact packaging; 3 ruggedized cases
• Standard 2 year warranty
SPECIFICATIONS ARE SUBJECT TO CHANGE WITHOUT NOTICE.
(English)
Mechanical
Reflector | 98 cm Elliptical Antenna, offset feed |
Platform Geometry | Elevation over Azimuth |
Deployment Sensors | GPS antenna |
Compass ± 2º | |
Tilt sensor ± 0.1º | |
Azimuth | ± 175º |
Elevation | 0 – 90º |
Elevation Deploy Speed | Variable, 3º/sec typ. |
Azimuth Deploy Speed | Variable, 3º/sec typ. |
Peaking Speed | 0.1º/sec |
Environmental
Wind loading | |
Operational (no ballast) | 50 km/h (30 mph) |
Operational (with ballast) | 72 km/h (45 mph) |
Temperature | |
Operational | -30º to 60º C (-22º to 140º F) |
Survival | -40º to 65º C (-40º to 149º F) |
Water Ingress Rating | IP-66 |
Electrical
Rx & Tx Cables | 2 RG6 cables -10 m (33 ft) each |
Control Cables | |
Standard | 10 m (33 ft) Ext. Cable |
Optional | up to 60 m (200 ft) available |
Receive Transmit | |
Frequency ( GHz) | 10.70-12.75(1) 13.75-14.50 |
Feed Interface (Circular) | WR-75 WR-75 |
Midband Gain (+-0.2 dBi) | [email protected] GHz [email protected] GHz |
Antenna Noise Temp. (K) | 10º EL=53 / 20º EL= 39 / 30º EL= 32 Max. |
Sidelobe Envelope Co-Pol (dBi) | |
1.8º < Ø < 20º | 29 – 25 Log Ø |
20º < Ø < 26.3º | -3.5 |
26.3º < Ø < 48º | 32-25 Log Ø |
48º < Ø < 180º | -10 (typical) |
Cross-Polarization | > -30 dB in 1 dB Contour |
VSWR | 1.5:1 1.3:1 |
RF Interfaces
Radio Mounting | Feed Arm |
Coaxial | RG6U F Type to tripod base (N Type Optional) |
Physical
Case 1: Reflector | L: 109 cm (43” ) | W: 109 cm (43”) |
H: 29 cm (11.5”) | 28.6 Kg (63 lbs) | |
Case 2: Tripod/Feed arm | L: 122 cm (48”) | W: 58 cm (23”) |
H: 28cm (11”) | 27.7 Kg (61 lbs) | |
Case 3: Controller/AZ/EL | L: 44.5 cm (17.5”) | W: 80 cm (31.5”) |
H: 38 cm (15.5”) | 34 Kg (75 lbs) |
Motors
Electrical Interface | 24VDC | 8 Amp (Max.) |
Shipping Weights & Dimensions
Skid: 132 cm x 137 cm x 121.9 cm (52” x 54” x48”) 23.1 Kg (51lbs) |
Total weight of system in cases: 90.3 Kg (199 lbs) |
Total weight of system in cases on skid: 113.4 Kg (250 lbs) |
* The shipping weights/dims can vary for particular shipments depending on actual system confguration, quantity, packaging materials and special requirements
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