| 词条 | Atlas H-10 | |||||||||||||||
| 释义 |
The Atlas H-10 was the prototype for a four-seat cabin monoplane aircraft, registered N37463, designed by Max Harlow, which was flown in the United States shortly after World War II. HistoryThe Atlas H-10 had been constructed from the unfinished Harlow PJC-4 sporting monoplane which had been left uncompleted at the outbreak of the conflict. The water heater company Rheem Manufacturing Company briefly invested in the project as the PCC-10 (Pasadena City College Model 10) but did not pursue the business. Pasadena students completed the aircraft, and its first flight was on 4 October 1945 with a 220 hp Lycoming.[1] It was a low-wing cantilever monoplane of aluminum semi-monocoque configuration with retractable tailwheel undercarriage and powered by a variety of engines throughout its life. Originally powered by a Lycoming O-435, it was re-engined with two Continental O-300s driving contra-rotating propellers through a common gearbox and registered as the Mono-Twin. In turn, this arrangement was replaced with a Franklin 6AB and finally a Lycoming IO-720, each driving a single propellor. The cabin layout was also modified. Operational historyOnly the single H-10 was completed and flown. In the early 1970s it was based at Long Beach Airport in southern California. As of 2006, the aircraft was reportedly still in existence in a dismantled state in the hands of a Californian collector. Variants
Original design
Test aircraft
Redesignated production aircraft
Re-engined prototype with twin radial Specifications (with Continental engines){{aerospecs|met or eng?=eng |crew=one pilot |capacity=three passengers |length m=8.64 |length ft=28 |length in=4 |span m=10.90 |span ft=35 |span in=9 |dia m= |dia ft= |dia in= |height m= |height ft= |height in= |wing area sqm= |wing area sqft= |rot area sqm= |rot area sqft= |aspect ratio= |empty weight kg= |empty weight lb= |gross weight kg= |gross weight lb= |eng1 number=2 |eng1 type=Continental O-300 |eng1 kw=108 |eng1 hp=145 |eng1 kn= |eng1 lbf= |eng1 kn-ab= |eng1 lbf-ab= |eng2 number= |eng2 type= |eng2 kw= |eng2 hp= |eng2 kn= |eng2 lbf= |eng2 kn-ab= |eng2 lbf-ab= |max speed kmh=274 |max speed mph=170 |max speed mach= |cruise speed kmh= |cruise speed mph= |range km= |range miles= |endurance h= |endurance min= |ceiling m= |ceiling ft= |glide ratio= |climb rate ms= |climb rate ftmin= |sink rate ms= |sink rate ftmin= |armament1= |armament2= |armament3= |armament4= |armament5= |armament6= }}{{aircontent |related= |similar aircraft= |sequence= |lists= |see also= }} References1. ^{{cite journal|magazine=Air Progress Sport Aircraft|title=The Quiet Professor|page=83}} {{commons category|Atlas H-10}}
5 : Harlow aircraft|United States civil utility aircraft 1940–1949|Single-engined tractor aircraft|Low-wing aircraft|Aircraft first flown in 1945 |
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