Rolls-Royce RB108

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RB.108
RollsRoyceRB108.JPG
Preserved RB.108 at the Royal Air Force Museum Cosford
Type Turbojet
Manufacturer Rolls-Royce Limited
First run 1955
Major applications Short SC.1
Developed into Rolls-Royce RB145

The Rolls-Royce RB.108 was a British jet engine designed in the mid-1950s by Rolls-Royce specifically for use as a VTOL lift engine, i.e., an engine intended primarily for providing upwards thrust rather than for horizontal propulsion.

Design and development[edit]

Of a squat and compact design for mounting vertically, the RB.108 differed from conventional turbojet engines in having its bearings and oil system designed for prolonged operation in the vertical attitude. First bench-tested in 1955 by Alan A. Griffith, who had conceived the idea of a specialised lift jet in 1941, thrust was 2,130 lbf (966.15 kg) from a weight of 269 lb (122 kg), giving a thrust/weight ratio of 8:1.

Applications[edit]

The RB.108 was used in the Short SC.1, which used four for lift with an additional one mounted at an angle at the rear for propulsion, and the Mirage Balzac, which used eight vertically mounted RB.108s for lift. The Vereinigte Flugtechnische Werke (VFW) SG 1262 used five RB.108s, three mounted in tandem on the centreline, with one RB.108 either side.

The RB.108 was also the intended powerplant for several other VTOL aircraft designs, including one by Dornier.

A similar lift jet was designed by Bristol Siddeley, the BS.59, with a thrust of 8,000 lb the engine was intended for the projected Focke-Wulf Fw 260.[1]

Specifications (RB.108)[edit]

Data from Gunston and Flight International[2][3]

General characteristics

  • Type: Single-spool turbojet
  • Length: 46.5 in (118 cm)
  • Diameter: 20.8 in (53 cm)
  • Dry weight: 269 lb (122 kg)

Components

Performance

See also[edit]

Related development
Related lists

References[edit]

Notes[edit]

Bibliography[edit]

External links[edit]