Venga TG-10

The Venga TG-10 Brushfire was a military trainer aircraft developed in Canada in the late 1980s.[1][2] The sole prototype was destroyed in a fire without having flown. The TG-10 was a low-wing, single-engine jet with seating in tandem for the pilot and instructor.[2] In general layout, it resembled the Northrop F-5 but had twin, outwardly-canted tail fins.[2] Construction was of composite materials throughout.[2][3] Announced to the public at the 1987 Paris Air Show,[4] the key selling point of the design was its low cost,[3] offering the performance of competing jet trainers at the cost of a turboprop trainer.[4] Venga Aerospace claimed letters of interest from five countries, involving up to 160 aircraft.[5] A single-seat ground-attack version[2][3] and a UAV version[6] were also considered.

TG-10 Brushfire
Role Military Jet Trainer
National origin Canada
Manufacturer Venga Aerospace Systems, Toronto
Status cancelled after sole prototype destroyed
Primary user None
Number built 1

Venga hoped to be able to enter the design in the USAF's JPATS competition,[7] but this did not transpire. Finance proved an ongoing problem for the project,[3] despite a partnership with Chinese firm Baosteel announced in 1994,[8] as the first prototype was nearing completion. At the time, Venga still claimed "soft orders" for 86 aircraft from five customers.[5] The aircraft was destroyed in a fire in May 1998,[9] and no further work was undertaken.[10] However, as recently as 2004, Venga hoped to relaunch the project.[6]


Specifications (prototype, as designed)

Data from Jane's All the World's Aircraft 1987–88, p.35

General characteristics

  • Crew: Two, pilot and instructor
  • Length: 11.89 m (39 ft 0 in)
  • Wingspan: 8.23 m (27 ft 0 in)
  • Height: 4.04 m (13 ft 3 in)
  • Wing area: 12.5 m2 (135 sq ft)
  • Empty weight: 1,288 kg (2,840 lb)
  • Gross weight: 2,645 kg (5,832 lb)
  • Powerplant: 1 × General Electric J85-GE-5 , 13.0 kW (2,925 hp)

Performance

  • Maximum speed: 899 km/h (558 mph, 485 kn)
  • Range: 1,760 km (1,094 mi, 951 nmi)
  • Rate of climb: 35.6 m/s (7,000 ft/min)

Armament

  • One centreline and four underwing pylons, each with capacity of 180 kg (400 lb)[5]

Notes
  1. Taylor 1989, p.947
  2. Jane's All the World's Aircraft 1987–88 p. 34
  3. Hatch 1988, p.56
  4. "Venga unveiled" 1987, p.11
  5. Air International May 1994, p.281.
  6. "Venga Enters Development Agreement with ACWI to Provide Flight and Combat Support Services for U.S. Military" 2004
  7. "USAF starts work on trainer requirement" 1989, p.13
  8. "China/Canada sign for trainer venture" 1994, p.11
  9. "Venga settles fire lawsuit" 2004
  10. Venga 2007, p.2

References
  • "Airdata File:Venga Aerospace TG-10 Brushfire". Air International. Vol. 46 no. 5. Stamford, UK: Key Publishing. May 1994. p. 281. ISSN 0306-5634.
  • "China/Canada sign for trainer venture". Flight International. 2–8 March 1994. p. 11. Retrieved 2008-12-30.
  • Hatch, Paul (13 August 1988). "Military Aircraft of the World". Flight International. pp. 22–80.
  • Jane's All the World's Aircraft 1987–88. London: Jane's Publishing. 1987.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
  • "USAF starts work on trainer requirement". Flight International. 28 October 1989. p. 13. Retrieved 2008-12-30.
  • Venga Aerospace Systems (2007). "Management's discussion and analysis" (PDF). Archived from the original (PDF) on 2011-06-07. Retrieved 2008-12-30. Cite journal requires |journal= (help)
  • "Venga Enters Development Agreement with ACWI to Provide Flight and Combat Support Services for U.S. Military". Business Wire. 18 June 2004. Retrieved 2008-12-30.
  • "Venga settles fire lawsuit" (Press release). 9 January 2004. Retrieved 2008-12-30.
  • "Venga unveiled". Flight International. 27 June 1987. p. 11. Retrieved 2008-12-30.
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