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The SPAS 13 was a development of the earlier SPAS 1 and was designed to demonstrate the advantages of a spherical airship. The 43 ft (13.11 m) diameter spherical envelope is made of
Spectra fabric with an inner helium containing envelope of
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piston engines on external struts, four vanes behind each engine are used to provide control by deflecting the thrust.
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45 ft 0 in (13.72 m) includes landing gear
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The SPAS 13 is powered by two 50 hp (37 kW)
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3-bladed, 6 ft 0 in (1.83 m) diameter
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255:Brassey's World Aircraft & Systems Directory
290:This article on an aircraft of the 1990s is a
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203:19.0 mph (30.6 km/h, 16.5 kn)
176:piston engine, 50 hp (37 kW) each
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197:30 mph (48 km/h, 26 kn)
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346:1990s Canadian experimental aircraft
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148:43 ft 0 in (13.11 m)
84:demonstrator designed and built by
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259:. London, England: Brassey's.
251:Taylor, Michael J. H. (1996).
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166:2,403 lb (1,090 kg)
75:21st Century Airships SPAS 13
351:Aircraft first flown in 1994
294:. You can help Knowledge by
160:1,596 lb (724 kg)
16:Canadian semi-rigid airship
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77:is a Canadian semi-rigid
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127:General characteristics
88:of Newmarket, Ontario.
92:Design and development
101:film reinforced with
86:21st Century Airships
58:21st Century Airships
356:1990s aircraft stubs
236:Taylor 1996, p. 538
164:Max takeoff weight:
341:Airships of Canada
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38:Type of aircraft
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45:National origin
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67:13 May 1994
188:Performance
180:Propellers:
170:Powerplant:
142:1 passenger
30:Semi-rigid
335:Categories
210:References
174:Rotax 503
146:Diameter:
140:Capacity:
121:Data from
110:Rotax 503
22:SPAST 13
152:Height:
136:1 pilot
82:airship
49:Canada
35:airship
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103:Kevlar
79:helium
32:helium
215:Notes
134:Crew:
99:Mylar
27:Role
292:stub
261:ISBN
172:2 ×
73:The
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223:^
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316:t
309:v
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