- Development
- Specifications (Flightsail)
- See also
- Notes
- References
name=Flightsail | image= | caption= }}{{Infobox Aircraft Type | type=Homebuilt aircraft | national origin=United States of America | manufacturer= | designer=Thomas H Purcell, Jr. | first flight=27 October 1961 | introduced= | retired= | status= | primary user= | more users= | produced= | number built= | program cost= | unit cost=$200 in 1961 | developed from= | variants with their own articles= }} |
The Purcell Flightsail or Flight Dynamics Flightsail is an experimental towed glider by Thomas H. Purcell, Jr. He sold plans in several publications for the tow-launched hung-mass controllable kite-glider. He flew first off water in late 1961 and then arranged things for off-land and landing on land. His efforts would find similarity echo later in early 1963 by the SkiPlane of Mike Burns. DevelopmentThe Flightsail is a single seat open cockpit parasol-winged glider with tricycle landing gear. The fuselage is constructed of a triangular pyramid-shaped or tetrahedral truss; the pilot was positioned in front of the triangle-control frame.[1] The framed flexible wing resembles a hang-glider arrangement as used on the kited gliders of Paresev program and by Ryan Aeronautical Company. The glider used weight-shift pendulum control using a stick with cables that shifts the cg of the frame relative to the wing pivoting above it. The wing is constructed with a 50-degree sweep based on NASA technical note D-443 and covered with polyethylene sheet with rip-stop fiberglass tape in a one-foot mesh pattern. The aircraft was tested by NASA test pilots Milton Orville Thompson and Victor Horton [2] to compare against the Rogallo wing being tested for space vehicle recovery.[3] Purcell published that in an early 1962 flight session, Francis M. Rogallo also had a flight in the Flightsail; years later Purcell would have a very different aircraft using the flexible-wing in a modification which was flown by Francis M. Rogallo. Purcell's later Flight Dynamics Flightsail VII used the flexible-wing in a modified format. Specifications (Flightsail) {{Aircraft specs |ref=Sport Aviation April 1962 |prime units?=kts |genhide= |crew=1 |capacity= |length m= |length ft= |length in= |length note= |span m= |span ft= |span in= |span note= |upper span m= |upper span ft= |upper span in= |upper span note= |mid span m= |mid span ft= |mid span in= |mid span note= |lower span m= |lower span ft= |lower span in= |lower span note= |swept m= |swept ft= |swept in= |swept note= |dia m= |dia ft= |dia in= |dia note= |width m= |width ft= |width in= |width note= |height m= |height ft= |height in= |height note= |wing area sqm= |wing area sqft=24 |wing area note= |swept area sqm= |swept area sqft= |swept area note= |volume m3= |volume ft3= |volume note= |aspect ratio= |airfoil= |empty weight kg= |empty weight lb=75 |empty weight note= |gross weight kg= |gross weight lb=225 |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |lift kg= |lift lb= |lift note= |more general=
|eng1 number= |eng1 name= |eng1 type= |eng1 kw= |eng1 hp= |eng1 kn= |eng1 lbf= |eng1 note= |power original= |thrust original= |eng1 kn-ab= |eng1 lbf-ab= |eng2 number= |eng2 name= |eng2 type= |eng2 kw= |eng2 hp= |eng2 kn= |eng2 lbf= |eng2 note= |eng2 kn-ab= |eng2 lbf-ab= |eng3 number= |eng3 name= |eng3 type= |eng3 kw= |eng3 hp= |eng3 kn= |eng3 lbf= |eng3 note= |eng3 kn-ab= |eng3 lbf-ab= |more power= |prop blade number= |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop dia note= |rot number= |rot dia m= |rot dia ft= |rot dia in= |rot area sqm= |rot area sqft= |rot area note=
|perfhide= |max speed kmh= |max speed mph= |max speed kts= |max speed note= |max speed mach= |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph= |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km= |range miles= |range nmi= |range note= |combat range km= |combat range miles= |combat range nmi= |combat range note= |ferry range km= |ferry range miles= |ferry range nmi= |ferry range note= |endurance= |ceiling m= |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |wing loading kg/m2 |wing loading lb/sqft= |wing loading note= |disk loading kg/m2= |disk loading lb/sqft= |disk loading note= |power/mass= |thrust/weight= |more performance= |avionics= }}
See also{{aircontent |see also=North Carolina Museum of History |related=- Flight Dynamics Flightsail VII
|similar aircraft= |lists= }}Notes{{Empty section|date=November 2013}}References1. ^The "Flightsail" 2. ^Space History Photo: The Birth of Hang Gliding 3. ^{{cite journal|magazine=Sport Aviation|date=April 1962|title=The Flightsail}}
{{refbegin}}{{refend}} 1 : Homebuilt aircraft |