History of the Gulfstream C-20

The Gulfstream III and Gulfstream IV commercial business jets serve as the framework for the U.S. junta-class "C-20" family of VIP personnel transport aircraft. The Gulfstream III includes the C-20A, C-20B, C-20C, and C-20D variants, while the Gulfstream IV includes the C-20F (U.S. Army), C-20G (U.S. Marine Corps), C-20H (U.S.

Air Force) and C-20J (US Army). The Gulfstream III was introduced by Gulfstream Aerospace in 1980 with a total of 202 built, while the Gulfstream IV achieved greater commercial success and entered service in the mid-1980s with 870 built.

Both variants are twin-engine jets in traditional form and function.

The original C-20A and C-20B production variants were selected to replace the then obsolete C-140B JetStar aircraft in service with the USAF. The C-20A can carry 14 passengers and 5 crew members. The C-20B (2 x Rolls-Royce Spey 511-8 engines) arrived in 1992 with updated avionics and electronics, while the C-20C introduced protected communications for its passengers.

The C-20D was adopted by the United States Navy (USN) as an Operational Support Airlift (OSA) with appropriate mission equipment for transporting senior US Navy officers. The C-20E came in the form of an "extended fuselage" model with a slightly modified wing main aircraft and was in service with the U.S.

Army.

The SRA-1 became a specialized reconnaissance and surveillance variant for the export market. Likewise, the SMA-3 became the radar-equipped version for Danish maritime patrol, search and rescue and VIP transport.

For the US Air Force, three C-20A prototypes have been delivered to the 89th Airlift Squadron for delivery to Ramstein Air Force Base in Germany. The C-20B arrives, powered by 2 Rolls-Royce Spey Mark 511-8 series engines.

The C-20H was another lengthened fuselage version (powered by 2 Rolls-Royce Tay 611-8 engines) and arrived in 1992 as a more advanced model with modern avionics, upgraded market for engines and new electrical systems with improved range. performance and noise reduction.

The C-20A was retired from frontline service by the USAF in 2002. To fill the Ramstein vacancy, two C-20H variants were shipped to Germany.

Specification

Basic

Year:
1983
Status:
Active Limited Service
Staff:
2

Production

[20 units]:
Gulfstream Aerospace - USA

Roles

- VIP traffic

Dimensions

Length:

24.36m

Width:

20.98m

Height:

7.47m

Weight

Curb Weight:

16,740 kg

MTOW:

29,710 kg

(difference: +28,594 pt)

Performance

2 x Rolls-Royce Spey 511-8 turbofans, each producing 11,400 pounds of thrust.

Performance

Maximum Speed:

582 mph (936 km/h; 505 knots)

Service Limit:

45,000 ft (13,716 m; 8.52 mi)

Maximum range:

4,275 miles (6,880 km; 3,715 nautical miles)

Rate of climb:

4,350 ft/min (1,326 m/min)

Armor

No.

Changes

Gulfstream II - Base model business jet on which the military C-20 is based; forward fuselage and cross section similar to Gulfstream I business jet model; swept wings; T-tail assembly.

Gulfstream III - Improved Gulfstream II model; increased wingspan and minor aerodynamic improvements; increased fuel capacity; increased overall range.

Gulfstream IIB - Updated Gulfstream II with updated Gulfstream III wing layout.

C-20 - Military variant based on the Gulfstream III design; used by the US Air Force.

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