The TRACER from Navmar Applied Sciences Corporation is a dynamic, jet-engine, fixed-wing unmanned aerial vehicle built for multi-mission applications. The NASC TRACER™ offers a unique combination of technology and performance typically associated with more expensive alternatives.
Utilizing a customized Sonex Aerospace rolling airframe, The TRACER can be configured with a wide variety of payloads and systems. Multiple payload locations exist within the fuselage, under each wing, on each wing tip, on the centerline and within the nose radome.
The TRACER is designed to be a high performance, low-cost, reliable and field maintenance aircraft. The NASC design team has provided a low-risk, cost effective platform.
The TRACER from Navmar Applied Sciences Corporation is a dynamic, jet-engine, fixed-wing unmanned aerial vehicle built for multi-mission applications. The NASC TRACER™ offers a unique combination of technology and performance typically associated with more expensive alternatives.
Utilizing a customized Sonex Aerospace rolling airframe, The TRACER can be configured with a wide variety of payloads and systems. Multiple payload locations exist within the fuselage, under each wing, on each wing tip, on the centerline and within the nose radome.
The TRACER is purpose built for manned/unmanned teaming, high and low altitude operations, electronic warfare, insertion into contested airspace, reconnaissance, counter UAS, or communication relay missions and many other mission sets. The ability to rapidly reconfigure the TRACER also makes it an exceptional platform for research, development and testing advanced technologies.
NASC has carefully selected key avionics and systems to meet the ever evolving UAS challenges. The TRACER autopilot system leverages a modified version of the highly successful NASC Ground Control Station (GCS) currently used on the NASC TigerShark-XP and Teros unmanned aircraft.
A: Wingspan | 18′ (5.5m) |
B: Length | 16′ 6″ (5m) |
General Specifications | |
Engine | 258 lbf Thrust (2) |
Fuel Capacity | 100 gal. (378.5L) |
Empty Weight | 750 lbs.* (340kg)* |
Gross Weight | 1,450 lbs.* (Approx.) (658kg)* |
Payload Specifications | |
Max. Payload Weight | Up to 200 lbs.* (91kg)* |
Payload Capacity | Multiple payload locations – internal and external stores |
Frequencies | |
All Frequencies | Please contact NASC 215-675-4900 Ext. 4335 with your frequency questions. |
Flight Performance |
|
Service Ceiling | 26,000 ft.* (7,925m) MSL* |
Cruise Speed | 225 kts* (Approx.) |
Launch and Recovery | Conventional wheeled take-off and landing |
* Estimated – Actual value dependent on performance and/or integration of selected payload.
A: Wingspan | 18′ (5.5m) |
B: Length | 16′ 6″ (5m) |
General Specifications | |
Engine | 258 lbf Thrust (2) |
Fuel Capacity | 100 gal. (378.5L) |
Empty Weight | 750 lbs.* (340kg)* |
Gross Weight | 1,450 lbs.* (Approx.) (658kg)* |
Payload Specifications | |
Max. Payload Weight | Up to 200 lbs.* (91kg)* |
Payload Capacity | Multiple payload locations – internal and external stores |
Frequencies | |
All Frequencies | Please contact NASC 215-675-4900 Ext. 4335 with your frequency questions. |
Flight Performance |
|
Service Ceiling | 26,000 ft.* (7,925m) MSL* |
Cruise Speed | 225 kts* (Approx.) |
Launch and Recovery | Conventional wheeled take-off and landing |
* Estimated – Actual value dependent on performance and/or integration of selected payload.