220:"dress rehearsal" more than anything else. After takeoff for the final event on Sunday, the left engine threw a rod out the side of the block and created a tunnel of fire 4 feet (1.2 m) in diameter and about 15 feet (4.6 m) long. An onboard halon extinguishing system put the oil fire out and an uneventful single-engine landing was made. The engine installations were very compact and "close cowled", meaning the bodywork covering the engines had little clearance. The carbon fiber engine cowling was a structural component of the aircraft and as such had to be protected from heat-soak after shutdown. This was accomplished via two 2-stroke weed blowers immediately after the blades stopped turning, quickly followed by two air conditioner blowers attached to the air inlet "scuppers". The engine cowlings were lined with corrugated
229:
the majority of the time while airborne. Eventually it was determined that the oil drain holes were undersized in the rocker area of the heads as they were not intended to run at a constant high RPM in an automobile application. At race speeds, the engines were turning 8000 RPM, geared down to 2000 at the prop, the engines were expected to run at this level for the 15 minutes of the race. Fully half of the radiator inlet ducting was blocked off after the first test flight on March 22, 1991.
26:
228:
before fireup. This was due to the tight tolerances of the engine main bearings. Because methanol burns much cooler than gasoline, cooling was never an issue. Actually the cold nature of the methanol gave the team a problem with oil viscosity. The thick, graphite laden oil would "puke" overboard for
215:
in the race configuration. Methanol was the preferred fuel because no intercoolers were needed, and so the associated drag was eliminated. After the day's running had concluded the engines were again configured to burn gasoline to preclude the corrosive effects of methanol. The aircraft was entered
219:
The decision was made by Pond to attend Reno with the same engines used for flight testing. In fact, a vibrator was still attached to the left vertical stabilizer to initiate flutter as part of the planned flight test program. There was no expectation of victory the first year. It was viewed as a
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On
September 14, 1993, the Pond Racer was entered again and once more, piloted by Rick Brickert. During qualifying, the aircraft began leaking oil and suffered an engine failure leaving the right propeller unfeathered. Brickert pulled up, lowered the landing gear, and chose to perform a
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The aircraft made its debut at the 1991 Reno air races having been flown from the Scaled
Composites factory under escort. Gasoline was used as the fuel for the flight to Reno as this gave a greater range. The onboard engine control computers were replaced with equipment for metering
216:
in the Silver class and qualified at 400 mph (640 km/h), flown by experienced test pilot Rick
Brickert. The aircraft developed mechanical problems before the race was officially started and dropped out as a DNS.
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to produce 1,000 hp (750 kW). However, those fitted to the Pond Racer only ever achieved a peak of around 600 hp (450 kW). The engines drove 4-bladed propellers via propeller speed reduction units.
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Bob Pond commissioned the design with the idea of developing a modern aircraft that could compete with the vintage warbirds in the
Unlimited Class at the Reno air races. Bob Pond was concerned that each year at the
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of .007 thickness. Airflow was vital to structural integrity. Conversely, the powerplant units had to be preheated to nearly
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by retracting the gear again. The aircraft overshot a smooth landing area and crashed in rough terrain, killing the pilot.
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automobile engine. The engines were originally developed for auto racing and were
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that would be as fast and spectacular in the air as the warbirds.
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Mormillo, Frank B. (January 1994). "Unfulfilled
Promises".
385:. Vol. 120, no. 12. December 1993. p. 31.
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airliners.net Scaled
Composites 158 Pond Racer - Untitled
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463:. Vol. 118, no. 11. pp. 106–115.
342:400.0 mph (643.8 km/h, 347.6 kn)
258:Specifications (Performance 1991 Reno meeting)
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193:engines were chosen. These were based on the
1402:(vice president/general manager, test pilot)
567:Rutan Aircraft Factory and Scaled Composites
501:. Vol. 46, no. 1. pp. 47–51.
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1414:(director of flight operations, test pilot)
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478:Jane's All The World's Aircraft 1991–92
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480:. Coulsdon, UK: Jane's Defence Data.
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1470:Twin piston-engined tractor aircraft
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531:A WAV file of the Pond Racer fly-by
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1450:1990s United States sport aircraft
285:20 ft 0 in (6.10 m)
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453:Garrison, Peter (November 1991).
379:"Pond Racer Destroyed in Crash".
327:, 600 hp (450 kW) each
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177:The airframe was constructed of
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427:"Aerofiles information - Rutan"
745:Rocketcraft (as subcontractor)
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136:) was a twin-engine twin-boom
114:September 14, 1993 (Destroyed)
1:
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317:4,140 lb (1,878 kg)
311:3,500 lb (1,588 kg)
241:as part of the test program.
1465:Aircraft first flown in 1991
1420:(SpaceShipOne sole investor)
406:"AIRPLANE PAGE - Reno races"
233:was the initial test pilot.
130:Scaled Composites Pond Racer
7:
663:Virgin Atlantic GlobalFlyer
641:Aircraft (as subcontractor)
476:Lambert, Mark, ed. (1991).
425:K.O. Eckland (2008-02-13).
237:also flew the plane as did
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140:developed for Bob Pond by
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916:Mojave Aerospace Ventures
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687:Technology demonstrators
829:Spirit of Steve Fossett
575:Aircraft (main designs)
569:aircraft and spacecraft
305: in (7.741 m)
270:General characteristics
752:McDonnell Douglas DC-X
1408:(manager, test pilot)
911:The Spaceship Company
521:Mojave Virtual Museum
358:Lambert 1991, p. 474.
226:operating temperature
132:(Company designation
265:Unfulfilled Promises
766:Spaceflight program
325:Electramotive VG-30
179:composite materials
152:Reason for creation
33:General information
1455:Twin-boom aircraft
1390:(former president)
1460:Mid-wing aircraft
1445:Scaled Composites
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924:
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668:Williams V-Jet II
498:Air International
245:Problems and loss
146:Scaled Composites
126:
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95:Introduction date
54:Scaled Composites
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847:Stratolaunch Roc
814:White Knight Two
785:White Knight One
773:Programs / Ships
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1400:Mike Melvill
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780:SpaceShipOne
658:Toyota TAA-1
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409:. Retrieved
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239:Steve Hinton
235:Mike Melvill
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199:turbocharged
183:carbon fiber
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163:P-51 Mustang
155:
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103:First flight
81:Registration
72:Number built
49:Manufacturer
333:Performance
321:Powerplant:
291:25 ft
195:Nissan VG30
1434:Categories
1418:Paul Allen
1388:Doug Shane
1382:Burt Rutan
797:Enterprise
732:(uncrewed)
726:(uncrewed)
612:Pond Racer
582:VariViggen
432:2009-07-08
411:2009-07-08
347:References
231:Dick Rutan
142:Burt Rutan
65:Burt Rutan
19:Pond Racer
1384:(founder)
730:Model 396
724:Model 395
648:Adam A500
632:Model 401
617:Boomerang
507:0306-5634
469:0015-4806
391:0015-4806
289:Wingspan:
263:Data from
134:Model 158
122:Destroyed
866:Tier One
213:methanol
165:and the
138:aircraft
60:Designer
859:flights
736:Vantage
719:Triumph
714:Grizzly
709:Catbird
622:Proteus
607:Voyager
602:Long-EZ
597:Defiant
592:Quickie
587:VariEze
300:⁄
283:Length:
222:inconel
111:Retired
90:History
505:
484:
467:
460:Flying
389:
382:Flying
187:Kevlar
173:Design
85:N221BP
806:Unity
704:BiPod
277:Crew:
827:VMS
819:VMS
804:VSS
795:VSS
699:ATTT
694:ARES
673:X-38
503:ISSN
482:ISBN
465:ISSN
387:ISSN
323:2 ×
185:and
128:The
119:Fate
98:1991
38:Type
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896:17P
891:16P
886:15P
881:14P
876:13P
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