

Calspan continues to be the world leader in the use of In-Flight Simulators (IFS) for airborne Research, Development, Test & Evaluation (RDT&E). Calspan developed the first IFS in the 1940’s and now operates 5th-generation Learjet IFS aircraft. IFS were originally designed to assist with the development of manned aircraft. Today, IFS have found their niche as effective Unmanned Air Vehicle (UAV) Surrogates. Calspan Learjet IFS have and continue to play a major role in the development of Sense and Avoid (SAA) and Automated Aerial Refueling (AAR) UAV technologies, implementing actual UAV systems in an airframe that replicates the flight dynamics of the real aircraft, manned or unmanned.
The onboard programmable Fly-by-Wire (FBW), or Variable Stability System (VSS), is designed to take commands from either a pilot onboard the aircraft, a sensor operator in the main cabin, a UAV operator on the ground, or an autonomous control algorithm. The system architecture is set up such that extensive Validation and Verification (V&V) testing is not required before flight. 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 UAV and other airborne systems.
2041 Niagara Falls Blvd. | Niagara Falls, New York 14304
Tel: 716.236-1000 | Fax: 716.236-1001 | www.calspan.com
| Specifications: | |||||||||
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| Engines: | General Electric CJ-610 (2,870 lb thrust each) |
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| Weights: |
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| Max Range: | 1,100 NM | ||||||||
| Endurance: | ~2.5 hours | ||||||||
| NZ Limits: | +4.0/-1.0g (Non-VSS) | ||||||||
| +2.9/+0.15 g (VSS) |
