Vortech Shadow

The Shadow Two-Seat Gyroplane’s features are: a durable, high-strength airframe, dependable, FAA-certified Lycoming engine, certified disc brakes for superb ground handling, rugged gearbox-driven prerotator, large, expandable instrument panel, and a full electrical system for avionics and lights. It also takes off and lands in very short distances and operates exceptionally well at high altitudes. It’s size is easily reduced for storage in a garage or transported by trailer. It’s maximum speed is 100 mph.and its cruising speed is 75 mph. Shadow kit minus engine and instruments in 2001: $15,750

Engine: Lycoming O-320, 150 hp
Disk span: 29 ft
Disk area: 660 sq.ft
Height: 8.5 ft
Length: 13 ft
Empty wt: 750 lbs
Gross wt: 1290 lbs
Fuel cap: 12 USG
Max speed: 100 mph
Cruise speed: 75 mph
Range: 100+ sm
ROC: 1500 fpm
Take-off dist: 125 ft
Landing dist: 25 ft
Service ceiling: 18,000 ft
Seats: 2

Vortech Skylark 1

Developed from the G-1 design, pilots have expressed amazement at this craft’s stability and manoeuvrability. The Skylark can be flown in the Experimental Aircraft category. Although this is one of the more affordable homebuilts, the airframe and all of its major components have been designed for quality, dependability and durability.

Full instrumentation Skylark kit minus engine and instruments: $19,995 in 2001.
Skylark construction plans in 2001:
Reduced-size prints (11″ x 17″ format): $75 (add $6 postage U.S. or $16 foreign)
Full size prints (18″ x 24″ format): $175 (add $7 postage U.S. or $22 foreign)

Features of the Skylark:

  • Full helicopter flight: vertical take-offs & landings; forward, backward & sideward flight; hovering.
  • Standard helicopter control system
    -All-aluminum main- & tail-rotor blades
  • Aircraft-grade steel & aluminum airframe & major components, plus all AN hardware
  • Full instrumentation

Engine Rotax 582, 65 hp
Main Rotor Diameter 19 ft
Disk area: 283 sq.ft
Tail Rotor Diameter 3 ft 6 in
Height 7 ft
Length 17 ft 6 in
Empty Weight 350 lbs
Gross Weight 725 lbs
Payload Weight 375 lbs
Fuel cap: 10 USG
Power Loading 10.8 lbs/hp
Disc Loading 2.5 lbs/sq ft
Maximum Speed 95 mph
Cruise Speed 70 mph
Rate Of Climb 1,000 fpm
Maximum Altitude 12,500 ft
Range: 120 sm
Seats: 1

Vortech G-1

The G-1 Ultrtalight Helicopter, created in the early 1970s by Art Weilage, was tested and sold as low-cost kits by Compcop, Inc. Vortech offers the original construction prints to hobbyists curious about this design, or who want to study the concept as inspiration for a design of their own.

Developed, tested and sold in the 1970’s by Compcop, the G-1 was designed to fill the need for an affordable, easy-to-build ultralight helicopter. The entire helicopter can be built at home with ordinary tools at a low cost. No license is required to fly the G-1 because it is in the license-free “Ultralight Aircraft” category (see FAR Part 103). The construction manual provides all the details needed to build the G-1 with an engine of 40 h.p. or higher. The three McCulloch go-cart engines can be replaced with a single engine such as the Rotax 447. Aluminium construction.

Carries one person. Takes off and lands vertically. Flies forward, backward, sideward, & hovers.

Engines: 3 x McCulloch MC101 42 hp
Empty wt: 150 lb
Max wt: 420 lb
Rotor span: 12ft
Height: 5.5ft
Length: 12ft
Max speed: 80 mph
Cruise: 55 mph
Climb rate: 1,000 fpm
Range: 120 sm
Service ceiling: 10,000 ft
Seats: 1

Engine (typical) Kawasaki or Rotax, 40+ hp
Length 12 ft
Width 5.7 ft
Height 5 ft 6 in
Main rotor diameter 12 ft
Tail rotor diameter 2 ft
Empty weight 150 lbs
Gross weight 420 lbs
Useful payload 270 lbs
Fuel capacity 5 USgals
Fuel consumption 4 USgals/hour
Speed (max.) 80 mph
Altitude (max.) 10,000 ft asl

Engine: 3 x McCulloch, 9.5 hp
Rotor span: 3.66 m
MAUW: 190 kg
Empty weight: 66 kg
Fuel capacity: 19 lt
Max speed: 128 kph
Cruise speed: 80 kph
Fuel consumption: 12 lt/hr
Seats: 1
Plan price (1998): $34.95

von Hagan 1911 Aeroplane

Built by German immigrant Alexander von Hagan in Seattle, Washington, the machine had two sets of silk wings, an aluminium framework, two motors and three propellers. It weighed 600 pounds without the operator. One propeller was in the front, the second three-quarters back, and the third at the rear. One 40 hp motor ran the two front propellers and a smaller one of 35 hp powered the rear. Von Hagan was born in 1859 and served in the German army for 14 years.

von Cosel 1930 monoplane

In 1930 Carl T von Cosel, of Key West FL. Built a two-place cabin, high-wing monoplane amphibian, registered N879Y and powered by a 180hp LeRhône rotary engine.

The wings were never attached, so the plane was never flown. Some reports claimed that von Cosel, an undertaker by trade, kept his dead wife in it for an unstated period of time.

When he left Key West in 1940, he took the plane with him and both disappeared.

Volmer VJ-21 Jaybird

The Jarvis Jaybird design was acquired by Volmer Jensen as homebuilt project soon after World War II and became the VJ-21 Jaybird with retractable wheels and 75hp Continental A75 engine.

The 1947 Volmer Jaybird all-metal evolution features a pod nacelle with a pusher engine and has monowheel gear with outriggers on the wings. Reportedly more than 900 plans sold to builders through the 1960s.

A later owner (ca.1960) put a 125hp Continental C125 in, repositioned wings slightly lower and added small auxiliary fins.

VJ-21 Jaybird
Engine: 75hp Continental A-75
Wingspan: 45’0″
Length: 24’0″
Useful load: 500 lb
Max speed: 135 mph
Cruise speed: 110 mph
Stall: 35 mph
Range: 400 mi
Take-off run: 50′
Landing run: 150′
Seats: 2