Grob Strato 2C
| Strato 2C | |
|---|---|
 | |
| 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]
Data from Brassey's World Aircraft & Systems Directory 1999/2000[10]
General characteristics
- Crew: 4
- Length: 23.98 m (78 ft 8 in)
- Wingspan: 56.5 m (185 ft 4 in)
- Height: 7.76 m (25 ft 6 in)
- Wing area: 150 m2 (1,600 sq ft)
- Airfoil: DLR LH34[11]
- Empty weight: 6,650 kg (14,661 lb)
- Max takeoff weight: 13,350 kg (29,432 lb)
- Powerplant: 2 × Teledyne Continental TSIOL-550 , 300 kW (400 hp) each
- Powerplant: 1 × Pratt & Whitney Canada PW127 gas generator
Performance
- Maximum speed: Mach 0.56
- Cruise speed: 500 km/h (310 mph, 270 kn) at 24,000 m (78,740 ft) [a]
- Range: 18,100 km (11,200 mi, 9,800 nmi) [a]
See also
[edit]Related development
References
[edit]- a Estimated performance.
- ^ a b c d Taylor, 1996, p.173.
- ^ Jeziorski Flight International 31 January - 6 February 1996, p.66.
- ^ Galleithner 2004, p.552.
- ^ a b Bents et al. 1998, p.4.
- ^ Jeziorski Flight International 12–18 April 1995, p.16.
- ^ Taylor, 1999, p.152.
- ^ Jeziorski, Flight International 31 January - 6 February 1996, p.67.
- ^ Taylor, 1999, p.151.
- ^ Jeziorski, Flight International 10–16 July 1996, p.4.
- ^ Taylor, 1999, pp.151-152.
- ^ Lednicer, David. "The Incomplete Guide to Airfoil Usage". m-selig.ae.illinois.edu. Retrieved 16 April 2019.
Bibliography
[edit]- Bents David J., Mockler, Ted, Maldonado, Jaime, Harp, James L.Jr., King, Joseph F. and Schmitz. Paul C. Propulsion System for Very High Altitude Subsonic Unmanned Aircraft . NASA/TM—1998-206636. Cleveland, Ohio: NASA Lewis Research Centre, April 1998
- Galleithner, Hans. "High Altitude Research Aircraft as Further Examples of the Application of the Fibre Composite Technology". Aeronautical Research in Germany: From Lilienthal Until Today . Ernst-Heinrich Hirschel, Horst Prem, Gero Madelung. New York: Springer-Verlag, 2004. ISBN 3-540-40645-X.
- Jeziorski, Andrzej. "Strato 2C takes flight but funds stay low". Flight International. 12–18 April 1995.
- Jeziorski, Andrzej. "High and Dry". Flight International. 31 January - 6 February 1996. pp. 66–67.
- Jeziorski, Andrzej. "DLR cancels Strato 2C contract". Flight International. 10–16 July 1996, p. 4.
- Taylor, M.J.H. Brassey's World Aircraft & Systems Directory: 1995/1997 Edition. London: Brassey's, 1996. ISBN 1-85753-198-1.
- Taylor, M.J.H. Brassey's World Aircraft & Systems Directory: 1999/2000 Edition. London: Brassey's, 1999. ISBN 1-85753-245-7.
External links
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