All posts by Bryan Swopes

About Bryan Swopes

Bryan R. Swopes grew up in Southern California in the 1950s–60s, near the center of America's aerospace industry. He has had a life-long interest in aviation and space flight. Bryan is a retired commercial helicopter pilot and flight instructor.

Neil Alden Armstrong (5 August 1930–25 August 2012)

Aviation, Space Flight, , , , , , , , , , , , , , , ,
Neil Alden Armstrong, Astronaut, The First Human to Set Foot on the Surface of The Moon. (NASA)

The following is the official NASA biography from the John H. Glenn Research Center:

National Aeronautics and Space Administration
John H. Glenn Research Center
Lewis Field
Cleveland, Ohio 44135

Neil A. Armstrong

Neil A. Armstrong, the first man to walk on the moon, was born in Wapakoneta, Ohio, on August 5, 1930. He began his NASA career in Ohio.

After serving as a naval aviator from 1949 to 1952, Armstrong joined the National Advisory Committee for Aeronautics (NACA) in 1955. His first assignment was with the NACA Lewis Research Center (now NASA Glenn) in Cleveland. Over the next 17 years, he was an engineer, test pilot, astronaut and administrator for NACA and its successor agency, the National Aeronautics and Space Administration (NASA).

As a research pilot at NASA’s Flight Research Center, Edwards, Calif., he was a project pilot on many pioneering high speed aircraft, including the well known, 4000-mph X-15. He has flown over 200 different models of aircraft, including jets, rockets, helicopters and gliders.

Armstrong transferred to astronaut status in 1962. He was assigned as command pilot for the Gemini 8 mission. Gemini 8 was launched on March 16, 1966, and Armstrong performed the first successful docking of two vehicles in space.

As spacecraft commander for Apollo 11, the first manned lunar landing mission, Armstrong gained the distinction of being the first man to land a craft on the moon and first to step on its surface.

Armstrong subsequently held the position of Deputy Associate Administrator for Aeronautics, NASA Headquarters, Washington, D.C. In this position, he was responsible for the coordination and management of overall NASA research and technology work related to aeronautics.

He was Professor of Aerospace Engineering at the University of Cincinnati between 1971-1979. During the years 1982-1992, Armstrong was chairman of Computing Technologies for Aviation, Inc., Charlottesville, Va.

He received a Bachelor of Science Degree in Aeronautical Engineering from Purdue University and a Master of Science in Aerospace Engineering from the University of Southern California. He holds honorary doctorates from a number of universities.

Armstrong is a Fellow of the Society of Experimental Test Pilots and the Royal Aeronautical Society; Honorary Fellow of the American Institute of Aeronautics and Astronautics, and the International Astronautics Federation.

He is a member of the National Academy of Engineering and the Academy of the Kingdom of Morocco. He served as a member of the National Commission on Space (1985-1986), as Vice-Chairman of the Presidential Commission on the Space Shuttle Challenger Accident (1986), and as Chairman of the Presidential Advisory Committee for the Peace Corps (1971-1973).

Armstrong has been decorated by 17 countries. He is the recipient of many special honors, including the Presidential Medal of Freedom; the Congressional Space Medal of Honor; the Explorers Club Medal; the Robert H. Goddard Memorial Trophy; the NASA Distinguished Service Medal; the Harmon International Aviation Trophy; the Royal Geographic Society’s Gold Medal; the Federation Aeronautique Internationale’s Gold Space Medal; the American Astronautical Society Flight Achievement Award; the Robert J. Collier Trophy; the AIAA Astronautics Award; the Octave Chanute Award; and the John J. Montgomery Award.

Armstrong passed away on Aug. 25, 2012 following complications resulting from cardiovascular procedures. He was 82.

August 2012

http://www.nasa.gov/centers/glenn/about/bios/neilabio.html

Neil Alden Armstrong, age 6
Neil Alden Armstrong, age 6
Ensign Neil A. Armstrong, United States Naval Reserve, 23 May 1952. (U.S. Navy)
Ensign Neil Alden Armstrong, United States Navy, circa 1951. (U.S. Navy)
Ensign Neil Alden Armstrong, United States Navy, circa 1951. (U.S. Navy)
Ensign Neil A. Armstrong, as wingman to Lieutenant (j.g.) Ernie Moore, is flying the second Grumman F9F-2 Panther, Bu. No. 125122 (marked S 116), assigned to VF-51, USS Essex (CV-9), 1951. (Naval Aviation Museum)
Ensign Neil A. Armstrong, as wingman to Lieutenant (j.g.) Ernie Moore, is flying the second Grumman F9F-2 Panther, Bu. No. 125127 (marked S 116), assigned to VF-51, USS Essex (CV-9), 1951. (Naval Aviation Museum)
3 September 1951, Ensign neil Armstrong was flying his Grumman F9F-2 Panther, Bu. No., 125122, escorting a photo reconnaissance aircraft over Koreawhen his airplane was damaged by enemy ground fire. At low altitude, he struck and anti-aircraft cable whoich further damaged the fighter and made it impossible to land. Armstrong was abl eto reach friendly territory and ejected safely. This photograph was taken a short time later. (U.S. Navy)
3 September 1951, Ensign Neil A. Armstrong was flying his Grumman F9F-2 Panther, Bu. No., 125122, escorting a photo reconnaissance aircraft over Korea when his airplane was damaged by enemy ground fire. At low altitude, he struck an anti-aircraft cable which further damaged the fighter and made it impossible to land. Armstrong was able to reach friendly territory and ejected safely. This photograph was taken a short time later. (U.S. Navy) 
NASA Engineering Test Pilot Neil A. Armstrong, 1958. (NASA)
NASA Engineering Test Pilot Neil A. Armstrong, 1958. (NASA) 
NASA test pilot Neil A. Armstrong dons a pressure suit before his first flight in teh North American Aviation X-15 hypersonic research rocketplane, at Edwards AFB, 30 November 1960. (NASA)
NASA test pilot Neil A. Armstrong dons a David Clark Co. MC-2 full-pressure suit before his first flight in the North American Aviation X-15 hypersonic research rocketplane, at Edwards AFB, 30 November 1960. (NASA)
Neil Armstrong with the first North American Aviation X-15A, 56-6670, on Rogers Dry Lake after a flight, 1960. (NASA)
Neil Armstrong with the first North American Aviation X-15A, 56-6670, on Rogers Dry Lake after a flight, 1960. Armstrong made seven flights in the X-15, including the longest, “Neil’s Cross Country”. (NASA)
NASA Research Test Pilot Neail A. Armstrong with teh Bell X-14 at NASA Ames Research Center, February 1964. (NASA)
NASA Research Test Pilot Neil A. Armstrong with the Bell X-14 at NASA Ames Research Center, February 1964. (NASA via Jet Pilot Overseas) 
Neil A. Armstrong during a training exercise near Cimmaron, new Mexico, June 1964. (NASA via Jet Pilot Overseas)
NASA Project Gemini astronaut Neil A. Armstrong during a field training exercise near Cimarron, New Mexico, June 1964. (NASA via Jet Pilot Overseas)
Astronauts David R. Scott, Pilot (left) and Neil A. Armstrong, Command Pilot (right) with U.S. Air Force pararescue jumpers at the end of the nearly disastrous Gemini 8 mission, 17 March 1966. (NASA)
Astronauts David R. Scott, Pilot (left) and Neil A. Armstrong, Command Pilot (right) with U.S. Air Force pararescue jumpers at the end of the nearly disastrous Gemini 8 mission, 17 March 1966. (NASA)
NASA Project Apollo Astronaut Neil A. Armstrong with a Bell Aerosystems Lunar Landing Research Vehicle, 1969. (Ralph Morse/Time Life Pictures/Getty Images)
NASA Project Apollo Astronaut Neil A. Armstrong with a Bell Aerosystems Lunar Landing Research Vehicle, 1969. (Ralph Morse/Time Life Pictures/Getty Images)
Neil Alden Armstrong, Mission Commander, Apollo 11, 16 july 1969. (NASA)
Neil Alden Armstrong, Mission Commander, Apollo 11, 16 July 1969. (NASA)
Neil Armstrong steps onto the Moon, 10:56 p.m. EDT, 20 July 1969. (NASA)
Neil Armstrong steps onto the Moon, 10:56 p.m. EDT, 20 July 1969. (NASA)
Neil Alden Armstrong inside the Lunar Module on the surface of the Moon, 20 July 1969. (NASA)
Neil Alden Armstrong inside the Lunar Module Eagle on the surface of The Moon, 20 July 1969. (Edwin E. Aldrin, NASA) 
Professor Neil A. Armstrong in his classroom at the University of Cincinnati College of Engineering, 1974. (Peggy Palange, UC Public Information Office)
Professor Neil A. Armstrong in his classroom at the University of Cincinnati College of Engineering, 1974. (Peggy Palange, UC Public Information Office) 
A bronze statue of Neil Alden Armstrong in front of the Hall of Engineering.
An 8-foot tall bronze statue of Neil Alden Armstrong, sculpted by Chas Fagan, sits in front of the Neil Armstrong Hall of Engineering at Purdue University, West Lafayette, Indiana.

© 2015, Bryan R. Swopes

5 August 1908

Aviation, , , , , , ,
Zeppelin LZ 4 over the Bodensee. (Archiv der Luftschiffbau Zeppelin GmbH)

5 August 1908: While on a 24-hour demonstration flight from its base at Lake Constance, down the Rhine to Strasbourg and return, the airship Zeppelin LZ 4 stopped for emergency repairs to one of its engines.

While moored at Flugfeld Stuttgart-Echterdingen, the airship was caught by a storm which tore it away from its mooring. It crashed and caught fire. LZ 4 was completely destroyed.

Airship LZ4 after destruction at Flugfeld Stuttgart-Echterdingen, 5 August 1908.

© 2015, Bryan R. Swopes

4 August 1971

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A prototype Agusta A109 Hirundo hovering in ground effect. (Agusta)

4 August 1971: At its Cascina Costa plant, near the Aeroporto di Milano-Malpensa, northwest of Milan, Italy, Agusta test pilot Ottorino Lancia made the first flight of the prototype Agusta A109 Hirundo, serial number 7101. Also on board was one of the helicopter’s designers, Paolo Bellevita.

The Agusta A109 is an 8-place, light, twin-engine helicopter with a four-blade, fully-articulated main rotor and retractable landing gear. It can be flown by one pilot and carry up to seven passengers. The helicopter is certified for flight in visual meteorological conditions. It was certified by Italy’s Ente Nazionale per l’Aviazione Civile (ENAC) on 28 May 1975, and by the U.S. Federal Aviation Administration the following month. The first production helicopters were delivered in 1976.

The original production variant A109 was 10.71 meters (35 feet, 2 inches) in length. The fuselage had a maximum width of 2.88 meters (9 feet, 5 inches) and the helicopter’s overall height was 3.30 meters (10 feet, 10 inches). The maximum gross weight was 2,450 kilograms, or 5,400 pounds.

The main rotor diameter of the A109 is 11.00 meters (36 feet, 1 inch), and turns counter-clockwise, as seen from above. (The advancing blade is on the helicopter’s right side.) In normal operation, the main rotor turns 365–385 r.p.m. (95–100%). In autorotation, the range is 346–424 r.p.m. (90–110%). The two-bladed semi-rigid tail rotor had a diameter of 2.03 meters (6 feet, 8 inches). It is positioned on the left side of the tail boom in pusher configuration. The tail rotor turns clockwise, when seen from the helicopter’s left side. (The advancing blade is below the axis of rotation.)

The A109 was powered by two Allison 250-C20B turboshaft engines. They are rated at 346 shaft horsepower (113% torque), each, for takeoff (five minute limit). With one engine inoperative (OEI), the maximum power of the remaining engine is 400 shaft horsepower (five minute limit) and 385 shaft horsepower, maximum continuous power.

The A109’s maximum speed (VNE) is 168 miles per hour (270 kilometers per hour). The maximum operating altitude is 15,000 feet (4,572 meters). The helicopter’s total useable fuel capacity is 550.0 liters (145.3 gallons).

A prototype Agusta A109 Hirundo in ground effect hover. (Agusta)

The A109 remains in production in both civil and military variants. It is produced in Italy by Leonardo S.p.A. (formerly, AgustaWestland) and in China by Jiangxi Change Agusta Helicopter Co., Ltd.

© 2019, Bryan R. Swopes

4 August 1960

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4 August 1960: NASA research test pilot Joseph Albert Walker set an unofficial world speed record when he flew the number one North American Aviation X-15, 56-6670, to 2,195 miles per hour (3,532.5 kilometers per hour). This was the 18th flight of the X-15 Program. It was 56-6670’s eighth flight and Walker’s fourth X-15 flight. The purpose of this test was to gradually increase the rocket plane’s speed toward its design limit.

Airdropped from the Boeing NB-52A Stratofortress mothership, 52-003, over Silver Lake, near the California-Nevada border, at 08:59:13.0 a.m., PDT, Walker fired the X-15’s two Reaction Motors XLR11-RM-13 rocket engines for 264.2 seconds. The X-15 accelerated to Mach 3.31 and climbed to a peak altitude of 78,112 feet (23,810 meters). [The two XLR11s were used as an interim powerplant until the Reaction Motors XLR99 was ready. The combined thrust of both LR11s was only slightly more than the idle thrust of the XLR99.]

Walker touched down on Rogers Dry Lake at Edwards Air Force Base, California, after a flight of 10 minutes, 22.6 seconds.

Joe Walker with X-15 56-6670 on Rogers Dry Lake. (NASA)

© 2016, Bryan R. Swopes

4 August 1950

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A U.S. Air Force Sikorsky H-5F lifts off during the Korean War. (U.S. Air Force)

4 August 1950: During the Battle of the Pusan Perimeter, wounded soldiers were evacuated from the battlefield by helicopter for the first time when a Sikorsky H-5F of Detachment F, 3rd Emergency Rescue Squadron,¹ Air Rescue Service, United States Air Force, flew Private 1st Class Claude C. Crest, Jr., U.S. Army, from the Sengdang-ni area to an Army hospital. By the end of combat in 1953, 21,212 soldiers had been medevaced by helicopters.

Only the second military helicopter, the H-5 was frequently flown overloaded and outside of its center of gravity limits. The helicopter was not armed, though the pilot normally carried an M1911 .45-caliber semi-automatic pistol, and the crewman, a .30-caliber M1 Carbine.

Eleven commercial Sikorsky S-51 helicopters had been purchased by the Air Force in 1947 and designated R-5F. This was later changed to H-5F. It was a four-place, single-engine helicopter, operated by one pilot. The cabin was built of aluminum with Plexiglas windows. The fuselage was built of plastic-impregnated plywood, and the tail boom was wood monocoque construction. The main rotor consisted of three fully-articulated blades built of metal spars and plywood ribs, covered with two layers of fabric. (All metal blades soon became available.) The three bladed semi-articulated tail rotor was built of laminated wood. The main rotor turned counter-clockwise, as seen from above. (The advancing blade is on the helicopter’s right.) Its normal operating range was 175–195 r.p.m. The tail rotor was mounted on the helicopter’s left side in a pusher configuration. It turned clockwise as seen from the helicopter’s left. (The advancing blade is below the axis of rotation.)

Sikorsky S-51 three-view drawing with dimensions. (Sikorsky Historical Archives)

The helicopter’s fuselage was 41 feet, 1¾ inches (12.541 meters) long. The main rotor had a diameter of 48 feet, 0 inches (14.630 meters) and the tail rotor diameter was 8 feet, 5 inches (2.565 meters),² giving the helicopter an overall length of 57 feet, ½ inch (17.386 meters) with rotors turning. It was 12 feet, 11–3/8 inches (3.947 meters) high. The tricycle landing gear had a wheel base of 10 feet, 1 inch (3.073 and the tread was 12 feet, 0 inches (3.658 meters). The S-51 had an empty weight of 4,050 pounds (1,837 kilograms) and maximum gross weight of 5,300 pounds (2,404 kilograms) below 1,000 feet (305 meters) MSL.³ Fuel capacity was 100 gallons (379 liters).

The H-5F was powered by an air-cooled, supercharged, 986.749-cubic-inch-displacement (16.170 liter) Pratt & Whitney R-985 AN-5 (Wasp Jr. T1B4 ) which was placed in the fuselage behind the crew compartment with the crankshaft vertical. The R-985-AN-5 was a direct-drive, nine-cylinder radial engine with a compression ratio of 6:1. It required 91-octane aviation gasoline and was rated at 450 horsepower at 2,300 r.p.m., Standard Day at Sea Level. The R-985 AN-5 was 48.00 inches (1.219 meters) long, 46.25 inches (1.175 meters) in diameter and weighed 684 pounds (310.3 kilograms) with a magnesium crankcase.

The H-5F had a maximum speed (VNE) of 107 knots (123 miles per hour/198 kilometers per hour). Range was 275 miles (443 kilometers). The service ceiling was 14,800 feet (4,511 meters). The absolute hover ceiling was 3,000 feet (914 meters).

Sikorsky H-5, Korea. (U.S. Air Force)
Sikorsky H-5, Korea. (U.S. Air Force)

¹ Reorganized as the 3rd Air Rescue Squadron 10 August 1950.

² An 8 foot, 9 inch (2.667 meter) all-metal two-blade tail rotor assembly became standard with the H-5G, and was available to retrofit earlier helicopters.

³ The maximum gross weight had to be reduced 150 pounds (68 kilograms) for each additional 1,000 feet of altitude.

© 2018, Bryan R. Swopes