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The Capella Javelin is a family of American open cockpit high wing tractor configuration conventional landing gear-equipped ultralight aircraft that were produced in kit form by Capella Aircraft of Austin Texas and intended for amateur construction. The single seat Javelin I was designed to comply with the American FAR 103 ultralight regulations including that category's maximum 254 lb (115 kg) empty weight.

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Made by Capella Aircraft Corporation.

Empty Weight Lb
240
Stall Speed Mph
26
Eng 1 Type
single cylinder
two-stroke aircraft engine
Ceiling Ft
12500
Fuel Capacity
5
Cruise Speed Mph
60
Introduced
1999
Status
Production completed
Span In
Gross Weight Lb
575
Span Ft
28
Crew
one
Range Nmi
120
Climb Rate Ftmin
400
Unit Cost
6000.0
US$6000 without engine
propeller
instruments or covering supplies
Height In
Avionics
none
Manufacturer
Capella Aircraft Corporation
Max Speed Mph
63
Eng 1 Name
Rotax 277
Wing Area Sqft
112
Height Ft
6
Origin
United States
National Origin
United States
Length Ft
18
Prime Units
imp
Similar Aircraft
*Kolb Firefly*Kolb Firestar*TEAM Airbike
Eng 1 Hp
28
Eng 1 Number
1
Length In
Category
Capella aircraft
United States ultralight aircraft 1990-1999

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