RS-15 HP Aircraft, LLC   


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General Details
Manufacturer: HP Aircraft, LLC
Plane Name:

RS-15

Classified as: Unclassified
Country Of Origin: U S A
Designer: R.E. Schreder
No. of Seats 1
No. Built 20
   
Performance:
L/DMax: 38 93 kph / 50 kt / 58 mph
   
MinSink: 0.64 m/s / 2.1 fps / 1.24 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.
15 49.2 10.5 113 200 440 226 500 426 940 40.57 8.3 90 200
Aspect ratio: 21.5
Airfoil: Wortmann 67-150 modified
Structure: all-metal except for foam, wing ribs and fiberglass pod.
Engine:

Comment:
The RS-15 has an innovative pod-and-boom desgin which originally was intended to convert into various configurations, with wingspans of from 13 to 20 m. being matched with booms o suitable length, two-place pods, etc. In the event, Schreder decided to go with the basic 15 m. single-seat version featuring a fiberglass cockpit pod and a six-inch-diameter tube for the boom. The wing is similar to that used for the HP-16. A number of significantly modified RS- 15メs have been built including Otto Zaunerメs One Yankee with his own design of fuselage and tailplane.


           

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