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Hoffman X-1

The Hoffman X-1 Sweet Patootie is an American homebuilt aircraft designed by Edward C. Hoffman, first flying on 24 February 1960.

Hoffman X-1
Role Homebuilt aircraft
National origin United States
Designer Edward C. Hoffman
First flight 24 February 1960

Design and development edit

The Hoffman "Sweet Patootie" is a single place, low-wing, conventional landing gear-equipped aircraft.[1]

Specifications (X1) edit

Data from Jane's All the World's Aircraft 1961–62[2]

General characteristics

Performance

  • Maximum speed: 125 mph (201 km/h, 109 kn)
  • Cruise speed: 120 mph (190 km/h, 100 kn)
  • Range: 200 mi (320 km, 170 nmi)
  • Rate of climb: 1,000 ft/min (5.1 m/s)

References edit

  1. ^ "Experimental Aircraft Fly-In". Flying Magazine: 36. November 1960.
  2. ^ Taylor 1961, pp. 266–267
  • Taylor, John W. R. (1961). Jane's All The World's Aircraft 1961–62. London: Sampson Low, Marston & Company.

External links edit

  • Image of a X-1

hoffman, this, article, orphan, other, articles, link, please, introduce, links, this, page, from, related, articles, find, link, tool, suggestions, june, 2015, sweet, patootie, american, homebuilt, aircraft, designed, edward, hoffman, first, flying, february,. This article is an orphan as no other articles link to it Please introduce links to this page from related articles try the Find link tool for suggestions June 2015 The Hoffman X 1 Sweet Patootie is an American homebuilt aircraft designed by Edward C Hoffman first flying on 24 February 1960 Hoffman X 1Role Homebuilt aircraftNational origin United StatesDesigner Edward C HoffmanFirst flight 24 February 1960 Contents 1 Design and development 2 Specifications X1 3 References 4 External linksDesign and development editThe Hoffman Sweet Patootie is a single place low wing conventional landing gear equipped aircraft 1 Specifications X1 editData from Jane s All the World s Aircraft 1961 62 2 General characteristicsCrew 1 Length 17 ft 6 in 5 33 m Wingspan 19 ft 0 in 5 79 m Height 10 ft 0 in 4 0 m Airfoil NACA 23015 Empty weight 616 lb 279 kg Gross weight 894 lb 406 kg Powerplant 1 Continental C90 horizontally opposed piston aircraft engine 90 hp 67 kW Performance Maximum speed 125 mph 201 km h 109 kn Cruise speed 120 mph 190 km h 100 kn Range 200 mi 320 km 170 nmi Rate of climb 1 000 ft min 5 1 m s References edit Experimental Aircraft Fly In Flying Magazine 36 November 1960 Taylor 1961 pp 266 267 Taylor John W R 1961 Jane s All The World s Aircraft 1961 62 London Sampson Low Marston amp Company External links editImage of a X 1 Retrieved from https en wikipedia org w index php title Hoffman X 1 amp oldid 1066505747, wikipedia, wiki, book, books, library,

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