Grob Strato 2C

From Wikipedia, the free encyclopedia
Jump to: navigation, search
Strato 2C
Grob G 850 Strato 2C D-CDLR in 2012.jpg
Grob G 850 Strato 2C based in Mindelheim-Mattsies
Role High Altitude Research Aircraft
Manufacturer Grob Aircraft
First flight 31 March 1995
Status Prototype only
Number built 1

The Grob Strato 2C was a German experimental high altitude research aircraft. Powered by two turbocharged piston engines and featuring an extremely long span wing of composite construction, one aircraft was built in the 1990s, but was abandoned despite setting a world altitude record for piston-engined aircraft on its last flight.

Development and design[edit]

In April 1992, the German Aerospace Center (Deutsches Zentrum für Luft- und Raumfahrt e.V - DLR) commenced a programme to develop an aircraft to carry out atmospheric, stratospheric and climatic research.[1] It chose Grob Aerospace to design and build an aircraft to meet these requirements, based both on its experience in use of composite material in aircraft structures together with its successful development of the Egrett surveillance aircraft, with the aircraft expected to be operational by 1996.[2]

In order to meet the requirement to operate at an altitude of 24,000 m (78,700 ft) for 48 hours,[3] Grob designed a twin-engined aircraft with a straight, very high aspect ratio wing of 56.5 m (185 ft 4½ in) span.[4] The wings featured winglets, and were mounted across the top of the fuselage which terminated in a T-tail configuration. The aircraft was designed to be crewed by two pilots, and could accommodate two scientists and associated mission equipment in a pressurised cabin. A galley, rest facilities and a toilet were provided.[1]

Unlike the Egrett, which was powered by a single turboprop engine, the Strato was powered by two wing-mounted pusher compound engines consisting of a turbocharged piston engine with the Gas Generator from a PW127 turboprop engine to provide a constant supply of pressurised air to the piston engine at high altitude. This had the advantage of maintaining power at high altitudes.[4] Each engine drove a 6 m (19 ft 8 in) diameter five-bladed propeller.[1]

Construction of the airframe moulds started mid-November 1992, with airframe construction beginning in April the following year, starting with the tailplane. The airframe was completed in 1994 and engine installation commenced.[1]

Operational history[edit]

The prototype first flew on 31 March 1995.[5] Costs overran, however, and the prototype, which was intended as a Proof of Concept aircraft with off the shelf equipment and a heavier wing structure than planned for the production aircraft,[6] was late and did not deliver the expected performance.[7] Despite setting a world altitude record for manned piston-engined aircraft of 18,552 m (60,897 ft) on 4 August 1995,[8] on its 29th and what turned out to be final flight, the programme was cancelled by the DLR in 1996.[9]

Specifications (Strato 2C)[edit]

Strato 2C.jpg

Data from Brassey's World Aircraft & Systems Directory 1999/2000[10]

General characteristics

Performance

See also[edit]

Related development

References[edit]

Notes[edit]

  • a Estimated performance.
  1. ^ a b c d Taylor, 1996, p.173.
  2. ^ Jeziorski Flight International 31 January - 6 February 1996, p.66.
  3. ^ Galleithner 2004, p.552.
  4. ^ a b Bents et al. 1998, p.4.
  5. ^ Jeziorski Flight International 12–18 April 1995, p.16.
  6. ^ Taylor, 1999, p.152.
  7. ^ Jeziorski, Flight International 31 January - 6 February 1996, p.67.
  8. ^ Taylor, 1999, p.151.
  9. ^ Jeziorski, Flight International 10–16 July 1996, p.4.
  10. ^ Taylor, 1999, pp.151-152.

Bibliography[edit]

External links[edit]