Javelin J-4 Peterson   


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General Details
Manufacturer: Peterson
Plane Name:

Javelin J-4

Classified as: Unclassified
Country Of Origin: U S A
Designer: Max A. Peterson
No. of Seats 1
No. Built 8
   
Performance:
L/DMax: 32 89 kph / 48 kt / 55 mph
   
MinSink: 0.70 m/s / 2.3 fps / 1.36 kt
   


 

Specifications:
Span Area Empty Weight Payload Gross Weight Wing Load Water Ballast
m ft sq.m sq.ft kg lb. kg lb. kg lb. kg
/sq.m
lb.
/sq.ft
kg lb.
14.94 49 11.71 126 260 574 105 230 365 804 31.17 6.38 0 0
Aspect ratio: 19.2
Airfoil: NACA 64(3)-618
Structure: all metal, except bottom half of fuselage is fiberglass.
Engine:

Comment:
The J-4 Javelin, a single ship capable of carrying a child behind the pilot features an aileronless wing with spoilers for glidepath control and ムspoileronsメ for roll control, the latter causing almost no adverse yaw. The wing spar is a chem-milled tube, and the airplane uses very few normal rivets, most fastenings being cost saving pop rivets. The fuselage is built around a steel tube frame, with a lower fiberglass shell bonded to aluminum sheet wrapped over the deck. The Javelin first flew in 1969. ATC.


           

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