Cessna Citation Hemisphere

The super-midsize jet project aimed at long-range performance

Overview

Cessna United States 2019–2019 $35 million (2018)

The Cessna Citation Hemisphere was announced as a large-cabin business jet designed for long-range missions. Intended to expand Cessna’s product line, it featured modern aerodynamics and advanced engines. The program was ultimately discontinued before certification.

Specifications

Units
Engine
2 × Snecma Silvercrest
Engine type
Turbofan
Thrust
2 × 12,000 lbf · 53 kN
Avionics
SmartView Synthetic Vision System
Wing tips
No winglets
Seats
12 economy · 14 business · 14 first
Crew
Cabin width
6 ft 0 in  ·  1.82 m
Cabin height
6 ft 1 in  ·  1.85 m
Cabin length
29 ft 0 in  ·  8.84 m
Exterior length
Tail height
Fuselage diameter
Wing span
Baggage volume
100 ft³  ·  2.8 m³
Gross weight
Empty weight
Max takeoff weight
Max landing weight
Max payload
Fuel capacity
Max cruise speed
516 kt  ·  594 mph  ·  956 km/h
Maximum speed
Cruise speed
Approach speed
Range
4,500 nm  ·  5,180 mi  ·  8,330 km
Fuel burn
Ceiling
Rate of climb
Takeoff distance
Landing distance
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Operational Context

Cessna Citation Hemisphere — proposed long-range business jet

The Hemisphere project was introduced in the mid-2010s as a clean-sheet large-cabin Citation design. It was planned to use advanced turbofan engines and composite structures to enhance efficiency. Development progressed through early design stages before engine supplier challenges emerged.

Projected cruise speed was approximately 450 knots (830 km/h), with a maximum takeoff weight near 40,000 pounds (18,140 kg). Range goals were around 4,500 nautical miles (8,330 km). The cabin was designed for up to 12 passengers in executive configuration.

Following delays and market reassessment, Textron Aviation canceled the program in the late 2010s. Although it did not reach production, the Hemisphere illustrated evolving expectations in the super-midsize business jet segment. The project remains part of Citation development history.