Sierra Nevada RAPCON-X

History of Sierra Nevada RAPCON-X

Sierra Nevada Corporation (SNC) unveils the "RAPCON-X," designed to meet ongoing U.S. intelligence-surveillance-reconnaissance (ISR) needs. Utilizing a Bombardier Global 6500 business jet as its foundation, the platform is equipped with essential systems, sensors, and workstations. Under the proposed arrangement, a contractor would own and operate the aircraft, providing maintenance, flight operations, and logistical support as part of the partnership.

The Global 6500 BizJet's design remains sleek and functional, featuring a sharp nose cone for superior cockpit visibility and modern avionics. Its unique wing design, with economical winglets and a "T-shaped" rear wing, ensures high-speed performance and efficient engine exhaust. Mounted midship and low on the fuselage, the aircraft boasts retractable landing gear for ground operations, along with antennas and sensors strategically placed throughout the fuselage.

Performance specifications include up to 14 hours of mission duration, an operating altitude of 45,000 feet, and a range of 6,000 nautical miles. Leveraging existing commercial aircraft reduces acquisition and operating costs while capitalizing on proven speed, altitude, and range capabilities. The platform's modular interior allows for easy upgrades to accommodate evolving technology and mission demands, enhancing its tactical versatility and effectiveness.

Specification

Foundation

Year of Operation: 2025

Origins: United States

Status: Under development

Crew: 14

Production: 0

Manufacturer: Sierra Nevada Corporation (SNC) - USA

Carrier: US

Roles

Airborne Early Warning (AEW): A specially equipped platform that provides command and control (C2) capabilities to Allied air forces on the battlefield.

Electronic Warfare (EW): Ability to actively deny adversaries electromagnetic (EM) spectrum and protect that spectrum for allied forces.

Search and Rescue (SAR): Ability to locate and evacuate personnel from potentially hazardous or dangerous areas, such as downed pilots at sea.

X-Plane (development, prototyping, tech demos): Aircraft designed for prototyping, technology demonstration, or research/data collection.

Notable Features

Radar Capability: Houses may house (via specialized variants) radars for searching, tracking, and attacking enemy elements.

Multi-engine: Include two or more engines to improve survivability and/or performance.

Wing sweep: The main plane or leading edge has retraction lines for improved high speed performance and handling.

Wings: Main aircraft covered with winglets for improved fuel efficiency and handling.

High-speed performance: Can accelerate to higher speeds than the average aircraft at the time.

High performance: The ability to fly and operate at higher altitudes than the average aircraft of the day.

Extended range performance: Ability to travel long distances using on-board fuel supplies.

Super performance: The design covers the three key performance categories of speed, altitude and range.

Seaport: Able to operate over the ocean and survive certain harsh marine environments.

Depression in crew members: Support the pressurization required for crew survival at higher operating altitudes.

Crew management: In addition to the pilot, the aircraft also employs additional crew members who specialize in specific functions on the aircraft.

Closed crew room: There are partially or fully enclosed crew work areas.

Scalable: Has retractable/retractable landing gear to maintain aerodynamic efficiency.

Camera equipment: Payload supports photographic devices that provide still and/or live image/video results.

Dimensions and Weight

Length: 99.4 feet (30.30m)

Width/span: 94.2 feet (28.70m)

Height: 25.6 feet (7.80m)

Cured weight: 52,183 lbs (23,670 kg)

MTOW: 99,506 lbs (45,135 kg)

Wgt Difference: +47,322 lbs (+21,465 kg)

Main aircraft structure

Monoplane: Designed to use a single main wing main aircraft; this is the most popular arrangement of main aircraft.

Install low: The main aircraft is mounted low on the side of the fuselage.

Swipe back: The floor plan features a swept wing on the leading edge of the main aircraft, which increases operating speed.

Performance

Installed: 2 Rolls-Royce Pearl non-afterburner turbofan engines, each producing 15,125 lbs of thrust.

Maximum speed: 690 km/h (1,110 km/h | 599 kn)

Cruising speed: 559 km/h (900 km/h | 486 knots)

Maximum speed difference: +130 km/h (+210 km/h | 113 kn)

Maximum: 51,001 feet (15,545 m | 10 km)

Area: 7,596 km (12,225 km | 22,641 nautical miles)

Armor

None. Mission-specific equipment associated with the onboard ISR role.