page_title: Caspar C 32
section_title: Specifications (C 32)
hierarchical_section_title: Caspar C 32 / Specifications (C 32)
caption_attribution_description: English: Caspar C 32 3-view drawing from Les Ailes August 19,1927
context_page_description: The Caspar C 32 was an aircraft developed in Germany for aerial spraying in the late 1920s. It was a single-bay biplane with staggered, equal-span wings that accommodated the pilot and a single passenger or observer in tandem open cockpits. A small, additional horizontal stabiliser was fitted near the top of the tall single tail fin above the main horizontal stabiliser.
context_section_description: Data from Jane's all the World's Aircraft 1928
  General characteristics
  Crew: 1
  Capacity: 897 kg (1,978 lb) disposable load
  Length: 9 m (29 ft 6 in)
  Wingspan: 15 m (49 ft 3 in)
  Height: 3.9 m (12 ft 10 in)
  Wing area: 53 m² (570 sq ft)
  Empty weight: 1,403 kg (3,093 lb)
  Gross weight: 2,300 kg (5,071 lb)
  Powerplant: 1 × Junkers L5 6-cylinder water-cooled in-line piston engine, 230 kW (310 hp)   for take-off; 210 kW (280 hp) continuous
  Propellers: 2-bladed fixed pitch propeller
  Performance
  Maximum speed: 180 km/h (112 mph; 97 kn) 
  Landing speed: 80 km/h (50 mph; 43 kn)
  Service ceiling: 3,700 m (12,100 ft)
  Rate of climb: 1.9 m/s (370 ft/min)
  Time to altitude: 1,000 m (3,300 ft) in 8.6 minutes
  Wing loading: 43.4 kg/m² (8.9 lb/sq ft)
  Power/mass: 0.0875 kW/kg (0.0532 hp/lb)
caption: Caspar C 32 3-view drawing from Les Ailes August 19,1927
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