Tag Archives: National Aeronautic Association

24 March 1939

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Jackie Cochran with her Beechcraft D17W, NR18562. (FAI)
Jackie Cochran with her Beechcraft D17W, NR18562. (FAI)

24 March 1939: During a 2 hour, 26 minute flight over southern California, Jacqueline Cochran established a U.S. National Altitude Record for Women of 9,160 meters (30,052 feet). She flew a Beechcraft D17W “Staggerwing,” serial number 164, registered NR18562.

A National Aeronautic Association official, Larry Therkelson, took the recording barograph from the airplane and sent it to the N.A.A. headquarters in Washington, D.C., for certification. The record had previously been held by Ruth Rowland Nichols.¹

“Were I to make the simple statement that I climbed to an altitude of thirty-three thousand feet, that statement in and of itself would mean nothing because I have often gone higher than that. But when I add that I did this in 1937 in a fabric-covered biplane without heating, without pressurization and without an oxygen mask, the elements of an accomplishment are added. I nearly froze; the pipestem between my teeth through which I tried to get an oxygen supply from a tank and connecting tube was inadequate for the purpose, and I became so disoriented through lack of oxygen that it took over an hour to get my bearings and make a landing. The difference between the pressure my body was accustomed to on the ground and the atmospheric pressure at 33,000 feet was such that a blood vessel in my sinus ruptured. All this was a part of the cumulative evidence that led up to cabin pressurization and and mandatory use of the oxygen mask above certain altitudes.”

— The Stars at Noon, by Jacqueline Cochran, Little, Brown and Company, Boston, 1954, Chapter IV at Pages 61–62.

According to the U.S. Centennial of Flight Commission, Jackie Cochran “. . . set more speed and altitude records than any other pilot.”

Beechcraft D17W Staggerwing NR18562, c/n 164, which Jackie Cochran used to set an altitude record, 24 March 1939. (Unattributed)
Beechcraft D17W Staggerwing NR18562, c/n 164, which Jackie Cochran used to set an altitude record, 24 March 1939, at the Beechcraft factory, Wichita, Kansas, 1937. (Beech Aircraft Corporation)

The Beechcraft Staggerwing got its name because its lower wing was placed ahead of the upper wing (negative stagger). It was a fast airplane for its time and set several speed and altitude records. The Beechcraft D17W was a special version of the D17 production model. Only two were built. Jackie Cochran purchased it from Beech for $20,145, and it had been delivered to her by famed aviator Frank Hawks.

The “Staggerwing” was a single-engine, four-place biplane with an enclosed cabin and retractable landing gear, flown by a single pilot. The basic structure was a welded tubular steel framework, with wood formers and stringers. The wings and tail surfaces were built of wood spars and ribs. The airplane was covered with doped fabric, except the cabin and engine, which were covered in sheet metal.

Beech Aircraft Corporation Model 17 “Staggerwings” under construction. (Beech B-111/U.S. Air Force)

The airplane was 26 feet, 10 inches (8.179 meters) long with a wingspan of 32 feet, 0 inches (9.754 meters) and overall height of 8 feet, 0 inches (2.438 meters). It had an empty weight of 2,540 pounds (1,152.1 kilograms) and loaded weight of 4,250 pounds (1,927.8 kilograms).

While most biplanes had staggered wings, the Staggerwing was unusual in having negative stagger. This not only increased the pilot’s field of vision, but improved the airplane’s stability in a stall. The leading edge of the Model 17 upper wing was 2 feet, 1–19/32 inches (0.65008 meters) aft of the lower wing. The leading edges had 0° 0′ sweep. Both wings had an angle of incidence of 5° 5′. The upper wing had no dihedral, but the lower wing had +1°. The mean vertical gap between the wings was 5 feet (1.52 meters), and the chord of both wings was 5 feet, 0 inches (1.524 meters). The total wing area was 269.5 square feet (25.04 square meters). The horizontal stabilizer had 0° incidence, while the vertical fin was offset 0° 43′ to the left of the airplane’s centerline.

Beech D17W NR18562. (Beechcraft)
Beechcraft D17W NR18562, c/n 164, carrying race number “13.” (Beech Aircraft Corporation)

The Staggerwing was offered with a selection of engines of different displacements and horsepower ratings. The standard Beechcraft D17S was equipped with an air-cooled, supercharged, 986.749-cubic-inch-displacement (16.170 liters) Pratt & Whitney Wasp Jr. A, a nine-cylinder radial engine producing 300 horsepower at 2,000 r.p.m at Sea Level. It had a maximum speed of 212 miles per hour (341 kilometers per hour), 670 mile (1,078 kilometer) range and service ceiling of 25,000 feet (7,620 meters).

The 1,343.804-cubic-inch-displacement (22.021 liter) Pratt & Whitney Wasp SC-G engine installed in Jackie Cochran’s D17W was an experimental version of the Wasp C with 5:4 propeller reduction gearing. It produced 600 horsepower at 2,850 r.p.m. for takeoff, and 525 horsepower at 2,700 r.p.m., up to 9,500 feet (2,896 meters). The SC-G never entered production.

Beechcraft D17W c/n 164, was impressed into military service at Tarrant Field, Texas, 12 March 1943. Assigned to the United States Army Air Corps, it was given the designation UC-43K Traveler and Air Corps serial number 42-107277. It was turned over to the Reconstruction Finance Corporation, 22 November 1944, for sale to the civil market. The airplane was now powered by a 971.930-cubic-inch displacement (15.927 liter) Wright R-975-5 Whirlwind nine-cylinder radial and was redesignated Beechcraft D17R. The Staggerwing was sold to the Carver Pump Company, Muscatine, Iowa, and registered NC50958.

The record-setting Beechcraft Staggerwing crashed at Avenger Field, Sweetwater, Texas, 15 December 1945.

Jackie Cochran's beechcraft D17W, NV18562, c/n 164, carrying the race number "33" circa 1937. (Unattributed)
Jackie Cochran’s Beechcraft D17W, NX18562, c/n 164, carrying the race number “33” circa 1937. (Unattributed)

¹ FAI Record File Number 12228: 8,761 meters (28,743 feet), 6 March 1931.

© 2019, Bryan R. Swopes

6 March 1990

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Completing its final flight, Lockheed SR-71A 61-7972, flown by Lieutenant Colonel Raymond E. Yeilding and Lieutenant Colonel Joseph T. Vida, arrives at Washington Dulles International Airport, 6 March 1990, where it was turned over to the Smithsonian Institution National Air and Space Museum.
Completing its final flight, Lockheed SR-71A 61-7972, flown by Lieutenant Colonel Raymond E. Yeilding and Lieutenant Colonel Joseph T. Vida, arrives at Washington Dulles International Airport, 6 March 1990, where it was turned over to the Smithsonian Institution National Air and Space Museum.

6 March 1990: On its final flight, Lieutenant Colonel Raymond E. (“Ed”) Yeilding and Lieutenant Colonel Joseph T. (“J.T.”) Vida established four National Aeronautic Association and three Fédération Aéronautique Internationale speed records with a Lockheed SR-71A Blackbird, U.S. Air Force serial number 61-7972.

Departing Air Force Plant 42 (PMD) at Palmdale, California, Yeilding and Vida headed offshore to refuel from a Boeing KC-135Q Stratotanker so that the Blackbird’s fuel tanks would be full before beginning their speed run. 972 entered the “west gate,” a radar reference point over Oxnard on the southern California coast, then headed east to Washington Dulles International Airport (IAD) at Washington, D.C.

The transcontinental flight, a distance of 2,404.05 statute miles (3,868.94 kilometers), took 1 hour, 7 minutes, 53.69 seconds, for an average of 2,124.51 miles per hour (3,419.07 kilometers per hour).

Ben Rich, director of Lockheed's Advanced Development Projects ("Skunk Works") congratulates LCOL Ed Yeilding and LCOL J.T. Vida on their record-setting flight. (Unattributed)
Ben Rich, director of Lockheed’s Advanced Development Projects (“Skunk Works”), congratulates LCOL Ed Yeilding  (center) and LCOL J.T. Vida on their record-setting flight. (© Tony Landis)

Intermediate closed-course records were also established: Los Angeles to Washington, D.C., 2,299.67 miles (3,700.96 kilometers), 1:04:19.89, averaging 2,144.83 m.p.h  (3,451.77 km/h).; Kansas City to Washington, D.C., 942.08 miles (1,516.13 km), 25:58.53, 2,176.08 m.p.h. (3,502.06 km/h); and St. Louis to Cincinnati, 311.44 miles (501.21 km), 8:31.97, 2,189.94 m.p.h. (3,524.37 km/h).

Flight record data for 972's record-setting transcontinental flight, prepared by V.A. Wright, ADP, LASC.
Flight record data for 972’s record-setting transcontinental flight, prepared by V.A. Wright, Advanced Development Projects, Lockheed Aeronautical Systems Company.

Screen Shot 2015-03-05 at 10.20.01Screen Shot 2015-03-05 at 10.21.35Screen Shot 2015-03-05 at 10.22.43Screen Shot 2015-03-05 at 10.23.55This same SR-71 had previously set a speed record from New York to London of 1:54:56.4, averaging 1,806.957 m.p.h. (2,908.015 km/h). (It had to slow for inflight refueling.) Next, 972 set a record flying London to Los Angeles, 5,446.87 miles (8765.89 km), in 3 hours, 47 minutes, 39 seconds, averaging 1,435.49 m.p.h. (2,310.19 km/h). It also established an altitude record of 85,069 feet (25,929 meters).

This was 61-7972’s final flight. The total time on its airframe was 2,801.1 hours.

61-7972 is on display at the Steven V. Udvar-Hazy Center, Smithsonian Institution National Air and Space Museum.

Lockheed SR-71A Blackbird 61-7972 at the Steven V. Udvar-Hazy Center, Smithsonian NASM
Lockheed SR-71A Blackbird 61-7972 at the Steven V. Udvar-Hazy Center, Smithsonian NASM

© 2016, Bryan R. Swopes

5 March 1962

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Convair B-58A-10-CF Hustler 59-2458, Cowtown Hustler, at the National Museum of the United States Air Force. (U.S. Air Force)
Convair B-58A-10-CF Hustler 59-2458, Cowtown Hustler, at the National Museum of the United States Air Force. (U.S. Air Force)

5 March 1962: Operation Heat Rise. Two Convair B-58 Hustler supersonic bombers from the 65th Bombardment Squadron, 43rd Bombardment Wing, Carswell Air Force Base, Texas, took off at sunrise and headed west to Los Angeles, California. Off the Pacific coast they refueled from a Boeing KC-135A Stratotanker, then headed east at maximum speed. They were to enter a radar starting gate at Los Angeles, but the radar did not pick them up so they returned to the tanker, topped off the fuel tanks again, then proceeded east once again. This time their entry was visually confirmed.

The crew of Cowtown Hustler checks the weather and files their flight plan at Carswell Air Force Base, Texas, before taking off on Operation Heat Rise, 5 March 1962. (U.S. Air Force)
The crew of Cowtown Hustler checks the weather and files their flight plan at Carswell Air Force Base, Texas, before taking off on Operation Heat Rise, 5 March 1962. From center, right, 1st Lieutenant John T. Walton, Captain Robert G. Sowers and Captain Robert MacDonald. (U.S. Air Force via Jet Pilot Overseas)

Both B-58s had been assigned a block altitude of Flight Level 250 to Flight Level 500 (between 25,000 and 50,000 feet, or 7,620 to 15,240 meters) by the Federal Aviation Administration, and all other aircraft were cleared from those altitudes along the course. The flight outbound from Los Angeles was at 50,000 feet (15,240 meters) at speeds above Mach 2.

Convair B-58A-10-CF Hustler 59-2485 in flight. (General Dynamics)
Convair B-58A-10-CF Hustler 59-2458 in flight. (General Dynamics)

Under normal conditions, the maximum speed of the B-58 was limited to a skin temperature of 115 °C. (239 °F.) to prevent the aluminum honeycomb skin panels from delaminating. For this speed run, Convair engineers had authorized a temperature of 125 °C. (257 °F.), which would allow the two bombers to exceed 1,400 miles per hour (2,253 kilometers per hour). Sensors were placed in the skin to monitor the temperature rise (which gave the operation its name: “Heat Rise”).

The first B-58, call sign “Tall Man Five-Five,” had a problem with the navigation radar and had some difficulty locating their tanker, but finally were able to. The B-58s descended to 25,000 feet over Kansas for the third refueling and over a 21-minute period, took on 8,500 gallons (321,760 liters) of fuel, climbed back to 45,000 feet (13,716 meters) and then continued on to New York.

One of the two B-58 bombers refuels from a Boeing KC-135A Stratotanker over Kansas during Operation Heat Rise, 5 March 1962. (U.S. Air Force)
One of the two B-58 bombers refuels from a Boeing KC-135A Stratotanker over Kansas during Operation Heat Rise, 5 March 1962. (U.S. Air Force)

The Cowtown Hustler ¹ crossed the radar gate at New York with an elapsed time of 2:00:58.71 for the West-to-East flight, averaging 1,214.65 miles per hour (1,954.79 kilometers per hour). The second B-58, Tall Man Five-Six, was one minute behind.

Passing New York, the two B-58 Hustlers proceeded over the Atlantic Ocean and rendezvoused with tankers for a fourth aerial refueling, then headed back west to Los Angeles. Shortly after passing New York, Tall Man Five-Six developed mechanical troubles and had to withdraw from the round-trip record attempt.

Once again over Kansas, Cowtown Hustler refueled for a fifth time then continued back to Los Angeles. The East-to-West leg from New York to Los Angeles was completed in an elapsed time of 2:15:50.08, averaging 1,081.81 miles per hour (1,741.00 kilometers per hour).

General Thomas Power, Chief of Staff, Strategic Air Command, congratulates Captain Rober G. Swoers and his crew after Operation Heat Rise.
General Thomas S. Power, Chief of Staff, Strategic Air Command, congratulates Captain Robert G. Sowers and his crew at Los Angeles Airport after Operation Heat Rise. The three airmen were awarded the Distinguished Flying Cross by General Power. John T. Walton is wearing his new captain’s bars.

The total elapsed time, Los Angeles–New York–Los Angeles, was 4 hours, 41 minutes, 14.98 seconds (4:41:14.98), for an average speed of 1,044.97 miles per hour (1,681.71 kilometers per hour). The crew and the airplane established three National Aeronautic Association (NAA) U.S. national records for Speed Over A Recognized Course.

At Los Angeles, the flight crew, Captain Robert G. Sowers, Pilot, Captain Robert MacDonald, Navigator, and Captain John T. Walton, were congratulated by General Thomas S. Power, Chief of Staff, Strategic Air Command, and each airman was awarded the Distinguished Flying Cross.

For the eastbound transcontinental flight, the crew won the Bendix Trophy, and for “the most meritorious flight of the year,” they were also awarded the Mackay Trophy. Their records still stand.

Screen Shot 2015-03-04 at 10.33.18Screen Shot 2015-03-04 at 10.34.10Screen Shot 2015-03-04 at 10.34.37Reportedly, the U.S. Air Force received more than 10,000 damage claims for windows that were broken by the sonic booms created by the two B-58 Hustlers as they flew across the country.

Today, the record-setting, trophy-winning airplane, Convair B-58A-10-CF 59-2458, the Cowtown Hustler, is on display at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio.

The Bendix and macKay Trophy-winning flight crew of Operation Heat Rise, left to right, Captain Robert G. Sower, pilot; Captain Robert MacDonald, navigator; First Lieutenent John Walton, Defense Systems. behind them is another B-58A, 59-2447.(U.S. Air Force)
The Bendix and Mackay Trophy-winning flight crew of Operation Heat Rise, left to right, Captain Robert G. Sowers, Pilot; Captain Robert MacDonald, Navigator; First Lieutenent John Walton, Defense Systems Operator. Behind them is another B-58A, 59-2447. Rapid Rabbit, flown by another crew, was destroyed 15 February 1962, three weeks before Operation Heat Rise. (U.S. Air Force via Jet Pilot Overseas)

Later on the same day, Cowtown Hustler‘s sister ship, B-58A-10-CF 59-2459, crashed on takeoff from Carswell AFB. According to an article published in the Fort Worth Star-Telegram, “The speedy bomber veered to the right on the takeoff run, slammed through a 10-foot chain link fence and disintegrated atop an ammunition bunker, about 75 yards short of Lake Worth.” Its crew, Captain Robert Eugene Harter, pilot, Captain Jack De Voll Jones, navigator, and First Lieutenant James Thomas McKenzie, defensive systems operator, were killed.² 59-2459 was the eleventh B-58 loss.

The Convair B-58A Hustler was a high-altitude Mach 2 strategic bomber which served with the United States Air Force from 1960 to 1970. It was crewed by a pilot, navigator/bombardier and a defensive systems operator, located in individual cockpits. The aircraft is a delta-winged configuration similar to the Convair F-102A Delta Dagger and F-106 Delta Dart supersonic interceptors.

The Hustler is 96 feet, 10 inches (29.515 meters) long, with a wing span of 56 feet, 10 inches (17.323 meters) and an overall height of 31 feet 5 inches (9.576 meters). The fuselage incorporates the “area rule” which resulted in a “wasp waist” or “Coke bottle” shape for a significant reduction in aerodynamic drag. The airplane’s only control surfaces are two “elevons” and a rudder, and there are no flaps.

The B-58’s delta wing has a total area of 1,542.5 square feet (143.3 square meters) and the leading edges are swept back at a 60° angle. The wing has an angle of incidence of 3° and 2° 14′ dihedral (outboard of Sta. 56.5).

The B-58A had an empty weight of 51,061 pounds (23161 kilograms), or 53,581 pounds (24,304 kilograms) with the MB-1 pod. The maximum takeoff weight was 158,000 pounds (71,668 kilograms).

The B-58A was powered by four General Electric J79-GE-5 axial-flow afterburning turbojet engines, suspended under the wings from pylons. This was a single-shaft engine with a 17-stage compressor and 3-stage turbine. It had a Normal Power rating of 9,700 pounds of thrust (43.148 kilonewtons). The Military Power rating was 10,000 pounds (44.482 kilonewtons), and it produced a maximum 15,600 pounds (69.392 kilonewtons) at 7,460 r.p.m., with afterburner. The J79-GE-5 was 16 feet, 10.0 inches (5.131 meters) long and 2 feet, 11.2 inches (0.894 meters) in diameter. It weighed 3,570 pounds (1,619 kilograms).

The bomber had a cruise speed of 544 knots (626 miles per hour/1,007 kilometers per hour) and a maximum speed of 1,147 knots (1,320 miles per hour/2,124 kilometers per hour/Mach 2.00) at 67,000 feet (20,422 meters). The B-58A had a combat radius of 4,225 nautical miles (4,862 statute miles/7,825 kilometers). Its maximum ferry range was 8,416 nautical miles (9,685 statute miles/15,586 kilometers).

The B-58 weapons load was a combination of Mark 39, B43 or B61 thermonuclear bombs. The weapons could be carried in a jettisonable centerline pod, which also carried fuel. The four of the smaller bombs could be carried on underwing hardpoints. There was a General Electric M61 20 mm rotary cannon mounted in the tail, with 1,200 rounds of ammunition, and controlled by the Defensive Systems Officer.

116 were built and they served the Strategic Air Command until January 1970 when they were sent to Davis-Monthan AFB, Tucson, Arizona for long-term storage.

The crew of Cowtown Hustler is presented the Bendix Trophy by A.P. Fontaine of the Bendix Corporation. Left to right, Sowers, MacDonald, Walton, Fontaine and Crew Chief, Master Sergeant Cockrell.
The crew of Cowtown Hustler is presented the Bendix Trophy by A.P. Fontaine, Director of Engineering, and later CEO, of the Bendix Corporation. Left to right, Captain Robert MacDonald, Captain John T. Walton, Captain Robert G. Sowers, Mr. Fontaine and 59-2458’s Crew Chief, Master Sergeant Cockrell.

The 19 minute, 38 second video below is a General Dynamics informational film about Operation Heat Rise. This video clip is longer than the time it took Cowtown Hustler to fly from Los Angeles, California, to the Grand Canyon in Arizona.

¹ “Cowtown” is a nickname for Fort Worth, Texas, where the B-58s were based, as well as several other American cities.

² Fort Worth Star-Telegram, Tuesday, 6 March 1962, Page 1 Column 8, and Page 4, Column 3

© 2019, Bryan R. Swopes

19–20 February 1979

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Professor Neil A. Armstrong in his classroom at the Iniversity of Cincinatti College of Engineering, 1974. (Peggy Palange, UC Public Informaton Office)
Professor Neil A. Armstrong in his classroom at the University of Cincinnati College of Engineering, 1974. (Peggy Palange, UC Public Information Office)

19–20 February 1979: Professor Neil Alden Armstrong of the University of Cincinnati College of Engineering, a member of the Board of Directors of Gates Learjet Corporation, former United States Navy fighter pilot, NACA/NASA research test pilot, Gemini and Apollo astronaut, and The First Man To Set Foot On The Moon, set five Fédération Aéronautique Internationale (FAI) and National Aeronautics Association class records for time to climb to an altitude and altitude while flying the prototype Learjet 28, serial number 28-001.

Professor Neil Armstrong and co-pilot Peter Reynolds in the cockpit of the record-setting Learjet 28, March 1979.
Professor Neil Armstrong and co-pilot Peter Reynolds in the cockpit of the record-setting Learjet 28.

Armstrong, with Learjet program test pilot Peter Reynolds as co-pilot, and with NAA observer Don Berliner aboard, flew the Learjet 28 to 15,000 meters (49,212.598 feet) in 12 minutes, 27 seconds over Kittyhawk, North Carolina, on 19 February.¹

On the same day, during a flight from Wichita, Kansas, to Elizabeth City, North Carolina, Armstrong flew the Learjet to 15,584.6 meters (51,130.577 feet), setting records for altitude, and for sustained altitude in horizontal flight.²  ³

The following day, 20 February 1979, flying from Elizabeth City, North Carolina, to Florence, Kentucky, Armstrong again set altitude and sustained altitude in horizontal flight, in a different class, by taking the Learjet to 15,585 meters (51,131.89 feet).⁴ ⁵

Learjet 28, serial number 28-001
Learjet 28, serial number 28-001. (NASA)

The Learjet 28 was a development of the Learjet 25 twin-engine business jet. It is operated by two pilots and can carry 8 passengers. The Model 28 used a new wing design. It was the first civil aircraft to be certified with winglets. The prototype first flew 24 August 1977, and it received certification from the Federal Aviation Administration 29 July 1979.

The Learjet 28 is 47 feet, 7.5 inches (14.516 meters) long with a wingspan of 43 feet, 9½ inches (13.348 meters) and overall height of 12 feet, 3 inches (3.734 meters). The wing area is 264.5 square feet (24.6 square meters) It has an empty weight of 7,895 pounds (3,581 kilograms) and maximum takeoff weight of 15,000 pounds (6,804 kilograms).

Gates Learjet 28 three-view illustration. (FLIGHT International, No. 3647, Vol. 115, 10 February 1979, Page 402)

The Learjet 28 is powered by two General Electric CJ610-8A turbojet engines. This is a single-shaft axial-flow turbojet, developed from the military J85. It has an 8-stage compressor section and 2-stage turbine. The CJ610-8A is rated at 2,850 pounds of thrust (12.68 kilonewtons) at 16,500 r.p.m., and 2,950 pounds (13.12 kilonewtons) at Sea Level, for takeoff (five minute limit).

The business jet has a cruise speed of 464 knots (534 miles per hour (859 kilometers per hour) at 51,000 feet (15,544.8 meters). The Learjet 28 has a maximum range of 1,370 nautical miles (1,577 statute miles/2,537 kilometers). The airplane’s maximum operating altitude is 51,000 feet (15,545 meters), the same as the record altitude. It can reach that altitude in less than 35 minutes.

The aircraft was limited by its older technology turbojet engines, and only five Learjet 28s were built.

gates Learjet 28 N128LR. (Business Aviation Online)

The first Learjet 28, serial number 28-001, has been re-registered several times. At the time of its FAI record-setting flights, it carried FAA registration N9RS. Later it was registered as N3AS. The most recent information shows it currently registered as N128LR.

The record-setting Learjet 28 is in the collection of the Armstrong Air & Space Museum, Wapakoneta, Ohio.

Neil Alden Armstrong, one of America’s most loved heroes, passed away 25 August 2012.

A bronze statue of Neil Alden Armstrong in front of the Hall of Engineering.
A bronze statue of Neil Alden Armstrong in front of the Hall of Engineering.

¹ FAI Record File Number 2652

² FAI Record File Number 8670

³ FAI Record File Number 8657

⁴ FAI Record File Number 2653

⁵ FAI Record File Number 2654

© 2019, Bryan R. Swopes

14 February 1932

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Ruth Rowland Nichols (FAI)

14 February 1932: Taking off from Floyd Bennett Field, Ruth Rowland Nichols flew Miss Teaneck, a Lockheed Vega 1 owned by Clarence Duncan Chamberlin, to an altitude of 19,928 feet (6,074 meters). This set a National Aeronautic Association record.

The airplane’s owner had flown it to 19,393 feet (5,911 meters) on 24 January 1932.

A contemporary newspaper reported:

RUTH NICHOLS SETS NEW ALTITUDE RECORD

     Ruth Nichols’ flight in a Lockheed monoplane powered with a 225 horsepower Packard Diesel motor to an altitude of 21,350 feet Friday had been credited to the Rye girl unofficially as a new altitude record for Diesel engines. A sealed barograph, removed from the plane, has been sent to Washington to the Bureau of Standards to determine the exact altitude figure.

—The Bronxville Press, Vol. VIII, No. 14, Tuesday, February 15, 1932, Columns 1 and 2

Ruth Nichols withwith Walter D. Wood, National Aeronautic Association, who is holding the sealed barograph, after setting FAI World Altitude Record. (FAI)

RUTH NICHOLS SETS AIR MARK

Aviatrix Beats Chamberlain [sic] Altitude Record

Sails 21,300 Feet High in Flying Furnace

Temperature Found to Be 15 Deg. Below Zero

     NEW YORK, Feb. 14.  (AP)—Ruth Nichols, society aviatrix, flew Clarence Chamberlin’s “Flying Furnace” to a new altitude record, on the basis of an unofficial reading of her altimeter.

     When she landed it registered 21,300 feet, while Chamberlin’s official record for the Diesel-motored craft was 19,363 feet.

     Miss Nichols took off at 4:15 p.m. from Floyd Bennett airport and landed an hour and one minute later after an exciting flight.

     She encountered temperatures of 15 degrees below zero, she said, and at 20,000 feet two of her cylinders blew out. At that height, too, she was forced to the use of her oxygen tank.

ENJOYED HER FLIGHT

     In addition to the sealed barograph, which was taken from the plane at once to be sent to Washington for official calibration, Miss Nichols had three altimeters, two of which went out of commission in the upper atmosphere. The unofficial reading was taken from the third altimeter.

     Despite her crippled engine and the fact that she had no brakes, she made a perfect landing and announced she had enjoyed the flight.

     He unofficial altimeter reading was greater than that of Chamberlin after his flight and it is believed the official calibration would establish the new record for planes of this type.

ADVISED BY CHAMBERLIN

     Chamberlin was present as her technical advisor, and he gave last-minute instructions as she stepped into the cockpit, wearing a heavy flying suit, lined boots, and a purple scarf wound about her head instead of a helmet.

     The plane carried 13 gallons of furnace oil, and one tank of oxygen. The regular wheels were changed smaller, lighter ones before the flight.

     Miss Nichols hold several records and has reached an altitude of 28,743 feet in a gasoline plane.

—Los Angeles Times, Volume LI. Monday, 15 February 1932, Page 3 at Column 3

Ruth Nichols’ Flight Record Confirmed

     Rye, N. Y., March 2—Miss Ruth Nichols, aviatrix, received notice from Washington today that her altitude flight from Floyd Bennett Airport, Barren Island, on Feb. 14 last in a Diesel-powered airplane to a height of 19,928 feet has set a new American Altitude record for that type of plane.

—Brooklyn Daily Eagle, Vol. XCI, No, 61, Page 2, Column 2

Miss Teaneck had been modified. The original Wright Whirlwind engine had been replaced by an air-cooled, 982.26-cubic-inch-displacement (16.096 liter) Packard DR-980 nine-cylinder radial diesel-cycle (or “compression-ignition”) engine. The DR-980 had one valve per cylinder and a compression ratio of 16:1. It had a continuous power rating of 225 horsepower at 1,950 r.p.m., and 240 horsepower at 2,000 r.p.m. for takeoff. The DR-980 was 3 feet, ¾-inch (0.933 meters) long, 3 feet, 9-11/16 inches (1.160 meters) in diameter, and weighed 510 pounds (231 kilograms). The Packard Motor Car Company built approximately 100 DR-980s, and a single DR-980B which used two valves per cylinder and was rated at 280 horsepower at 2,100 r.p.m. The Collier Trophy was awarded to Packard for its work on this engine.

Three-view drawing of the Lockheed Vega from a National Advisory Committee for Aeronautics publication. (NASA)

The Lockheed Vega was a very state-of-the-art aircraft for its time. The prototype flew for the first time 4 July 1927 at Mines Field, Los Angeles, California.

The Vega was very much a state-of-the-art aircraft for its time. It used a streamlined monocoque fuselage made of strips of vertical-grain spruce pressed into concrete molds and bonded together with cassein glue. These were then attached to former rings. The wing and tail surfaces were fully cantilevered, requiring no bracing wires or struts to support them. They were built of spruce spars and ribs, covered with 3/32-inch (2.4 millimeters) spruce plywood.

The Lockheed Vega 1 was flown by a single pilot in an open cockpit and could carry up to four passengers in the enclosed cabin. It was 27.5 feet (8.38 meters) long with a wingspan of 41.0 feet (12.50 meters) and height of 8 feet, 6 inches (2.59 meters). The total wing area (including ailerons) was 275 square feet (25.55 square meters). The wing had no dihedral. The leading edges were swept slightly aft, and the trailing edges swept forward. The Vega 1 had an empty weight of 1,650.0 pounds (748.4 kilograms) and a gross weight of 3,200 pounds (1,452 kilograms).

The early Vegas were powered by an air-cooled, normally-aspirated 787.26-cubic-inch-displacement (12.901 liter) Wright Whirlwind Five (J-5C) nine-cylinder radial engine. This was a direct-drive engine with a compression ratio of 5.1:1. The J-5C was rated at 200 horsepower at 1,800 r.p.m., and 220 horsepower at 2,000 r.p.m. It was 2 feet, 10 inches (0.864 meters) long, 3 feet, 9 inches (1.143 meters) in diameter, and weighed 508 pounds (230.4 kilograms).

The Vega had a cruising speed of 110 miles per hour (177 kilometers per hour) with the engine turning 1,500 r.p.m., and a top speed of 135 miles per hour (217 kilometers per hour)—very fast for its time. The airplane had a rate of climb of 925 feet per minute (4.7 meters per second) at Sea Level, decreasing to 405 feet per minute (2.1 meters per second) at 10,000 feet (3,048 meters). Its service ceiling was 15,900 feet (4,846 meters), and the absolute ceiling was 17,800 feet (5,425 meters). The airplane had a fuel capacity of 100 gallons (379 liters), giving it a range of 1,000 miles (1,609 kilometers) at cruise speed.

Twenty-eight Vega 1 airplanes were built by Lockheed Aircraft Company at the factory on Sycamore Street, Hollywood, California, before production of the improved Lockheed Vega 5 began in 1928 and the company moved to its new location at Burbank, California.

The techniques used to build the Vega were very influential in aircraft design. It also began Lockheed’s tradition of naming its airplanes after stars and other astronomical objects.

The first Lockheed Vega 1, NX913, Golden Eagle. (San Diego Air and Space Museum Archives)

© 2021 Bryan R. Swopes