Calspan has responded to the growing need for large scale testing of avionics
systems by developing a testbed based on a Gulfstream G-III aircraft. This system is specifically
designed to handle large Fire Control Radars, EO/IR sensors and heavy external stores. With more
than 65 years of experience in airborne Research, Development, Test & Evaluation (RDT&E), Calspan has
specifically modified and configured the airframe to support cost-effective flight testing of new airborne
sensors and/or systems for manned and unmanned aircraft alike. Calspan’s staff of experienced test pilots,
engineers, technicians, and mechanics are ready to assist customers with the safe and efficient design,
installation, and flight test of prototype airborne installations in the latest addition to the
Calspan fleet of test aircraft.
Basic Airframe Equipment:
- Bendix EFS-10 Electronic Flight Instrumentation System (EFIS)
- Triple Collins VHF-22C Comm Radios w/ 8.33 MHz spacing
- Dual Bendix VNS-41 Nav Radios with FM Immunity
- Triple Honeywell Laser Inertial Reference System (IRS)
- Dual Global GNS-XLS Flight Management System (FMS)/Global Positioning System (GPS)
- Dual Sperry Air Data Computers
- Honeywell Traffic Collision Avoidance System (TCAS) II
Experimental Provisions:
- External store
- Nominal 48 inch ground clearance from bottom of fuselage (38 inch minimum)
- 2,000 lb load carrying capability on centerline pylon
- Pylon wired and compatible with BRU-32, MAU-12, or MAU-40 ejector racks
- Universal radar mount in nose
- Accepts up to 40 inch diameter antenna
- Unique radome fabrication
- Electrical Power
- 65 KVA below 20,000 ft, 35 KVA above 20,000 ft
- 400 Hz and 60 Hz AC, 28 VDC
- Networking
- ARINC 429, ARINC 573, Mil-Std-1553, RS-232, Ethernet, USB, Serial
- Digital data recording
- Telemetry
- L-Band (including Freewave Data Link), S-band
- Cooling
- Programmable Autopilot
- Available volume
- 1,345 ft3 in main cabin, 157 ft3 in aft equipment bay
| Specifications: |
|
| Engines: |
Rolls Royce Spey MK511-8 (11,400 lb thrust each) |
| Weights: |
| Max Takeoff |
69,700 lb |
| Max Zero Fuel |
44,000 lb |
| Useful Load | 30,700 lb |
| Fuel Capacity | 28,300 lb |
|
| Max Range: |
3,400 NM |
| Endurance: |
7 hours |