- Design
- Operational history
- Specifications (Robertson Skylark SRX-1)
- References
- External links
name=Robertson Skylark SRX-1 | image= | caption= }}{{Infobox Aircraft Type | type=STOL aircraft | national origin=United States of America | manufacturer=Robertson Development Corp | designer=James L. Robertson | first flight=1955 | introduced= | retired= | status= | primary user= | more users= | produced= | number built= | program cost= | unit cost= | developed from= | variants with their own articles= }} |
The Robertson Skylark SRX-1 is a five place high performance STOL aircraft designed in the 1950s. It was intended to be operated out of {{convert|120|ft|m|0|abbr=on}} landing strips with {{convert|150|mph|km/h|0|abbr=on}} cruise speeds.[1] DesignThe aircraft was designed by James L. Robertson, son of William B. Robertson, Robertson Aircraft Corporation founder at the age of 27. The aircraft is designed to be stall-proof and spin-proof and is capable of a {{convert|25|mph|km/h|0|abbr=on}} minimum flight speed. It was also the first light aircraft in America to be designed to accommodate a turboprop engine.[2] The Skylark is all metal, with a steel tube internal structure. It incorporates shrouds, flaps, spoilerons, turbulator control, stabilators, elevances, and spinner duct cooling.[3] Operational historyTest flights were performed by aerobatic pilot Marion Cole. He featured the aircraft as part of his Cole Brothers airshows. The aircraft is able to take off in 100 feet. Specifications (Robertson Skylark SRX-1) {{Aircraft specs |ref=Experimenter |prime units?=kts |genhide= |crew=1 |capacity=4 passengers |length m= |length ft=30 |length in=6 |length note= |span m= |span ft=40 |span in= |span note= |height m= |height ft=7 |height in=10 |height note= |wing area sqm= |wing area sqft= |wing area note= |aspect ratio= |airfoil= |empty weight kg= |empty weight lb=2250 |empty weight note= |gross weight kg= |gross weight lb=3500 |gross weight note= |fuel capacity= |more general=
|eng1 number=1 |eng1 name=Continental GE260-2X |eng1 type= |eng1 kw= |eng1 hp=260 |prop blade number=2 |prop name=Hartzell HC-12x20-8C |prop dia m= |prop dia ft= |prop dia in= |prop 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=165 |max speed kts= |max speed note= |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= |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= |lift to drag= |wing loading kg/m2 |wing loading lb/sqft= |wing loading note= |power/mass= |thrust/weight= |more performance= |avionics= }}{{aircontent |see also= |related= |similar aircraft= |lists= }}
References1. ^{{cite journal|magazine=Flying Magazine|date=July 1954|page=37}} 2. ^{{cite journal|magazine=Experimenter|title=Project Skylark|date=April 1955}} 3. ^{{cite book|title=Survey of research projects in the field of aviation safety, Issue 6 Cornell University| author=Daniel and Florence Guggenheim Aviation Safety Center}}
External links- [https://books.google.com/books?id=zSADAAAAMBAJ&pg=PA60&source=gbs_ge_summary_r&cad=0#v=onepage&q&f=true "Plane Takes Off in 100 Feet.] Popular Science, July 1954, p. 60.
3 : United States civil utility aircraft 1950–1959|STOL aircraft|Aircraft first flown in 1955 |