On 2 November 1953, the Convair YF-102 prototype, 52-7994 was severely damaged when its Pratt & Whitney J57-P-11 engine flamed out during a test flight. The cause was traced to the engine’s Bendix fuel control. Dick Johnson was unable to restart the engine and was forced to make a gear-up landing in the desert, not far from Edwards Air Force Base. Johnson was seriously injured. The prototype was written off.
© 2016, Bryan R. Swopes
At 10:01 a.m., Saturday morning, Captain Freeman took off from Ellington Air Force Base, Houston, Texas. He was on the first of two planned training flights, flying a Northrop T-38A-50-NO Talon, 63-8188, Northrop serial number N.5535. The weather was reported as scattered clouds at 2,000 feet (607 meters), with visibility 7 miles (11.3 kilometers) in haze. He returned to the airfield at 10:38 for touch and goes, but was instructed to exit traffic pattern because of arriving aircraft.
At 10:46, Freeman called Ellington Tower, reporting that he was 5 miles (8 kilometers) southwest, inbound. He received no response and 30 seconds later, reported that he was breaking out to the east. The tower acknowledged this transmission and instructed Freeman to make another approach. At 10:47, Freeman called, “Roger, be about two minutes.” There were no further transmissions.
Ted Freeman’s T-38 struck a Lesser Snow Goose (Chen caerulescens) in the vicinity of the airport. These birds weigh between 4½ to 6 pounds (2.1–2.7 kilograms). The impact resulted in damage to the left side of the airplane’s forward canopy. Both engines flamed out.
Unable to reach runway at Ellington, Freeman turned away from the airfield to avoid buildings, lowered the landing gear and headed for an open field. At approximately 100 feet (30 meters), he fired his ejection seat. The altitude was too low to allow his parachute to open and Freeman was killed when he struck the ground.
The T-38 crashed at 10:48 a.m., 1 mile (1.6 kilometers) south of Ellington Air Force Base, between Highway 3 and the Gulf Freeway.
Investigators found blood and feathers in the cockpit. Suspecting a bird strike, a search was carried out and on 12 November, the remains of a snow goose along with fragments of the T-38’s canopy were found approximately 3 miles (4.8 kilometers) southeast of Ellington AFB, and about 4 miles (6.4 kilometers) from the crash site.
At 10:58 a.m., Charles Alden Berry, M.D., Chief of the Manned Space Flight Center Medical Operations Office, declared Captain Freeman dead at the scene. The Chief of the Astronaut Office, Deke Slayton, and Dr. Berry went to the Freeman home and made the formal notification to Mrs. Freeman.
Following an autopsy, Captain Freeman’s remains were transported to the Arlington National Cemetery, at Arlington, Virginia, for burial.
Theodore Cordy Freeman was born 18 February 1930 at Haverford, Pennsylvania. He was the fourth child of John T. Freeman, a carpenter, and Catherine Thomas Wilson Freeman. Ted Freeman attended Lewes High School, in Lewes, Delaware. He graduated in 1948, and was ranked academically third in his class. While still in high school, Freeman qualified for a private pilot’s license. He then studied at the University of Delaware at Newark.
While at the University of Delaware, Freeman received an appointment to the United States Naval Academy at Annapolis, Maryland, and entered as a midshipman, United States Navy, 17 June 1949. He graduated with a bachelor of science degree on 5 June 1953. Along with 129 of his classmates, Midshipman Freeman elected to be commissioned as a second lieutenant, United States Air Force.
Later that same afternoon, Second Lieutenant Theodore Cordy Freeman, United States Air Force, married Miss Faith Dudley Clark of Orange, Connecticut, at the First Presbyterian Church in Annapolis. They would have a daughter, Faith Huntington Freeman, born at Bryan, Texas, 18 July 1954.
Second Lieutenant Freeman trained as an Air Force pilot at Hondo and Bryan Air Bases in Texas. He was promoted to the rank of first lieutenant in February 1955 and awarded his pilot’s wings. Freeman was then sent for fighter training at Nellis Air Force Base, Las Vegas, Nevada. In 1955, Lieutenant Freeman was stationed in Okinawa. On his return to the United States, he was assigned to George Air Force Base in California.
In 1960, Freeman earned a master’s degree in aeronautical engineering at the University of Michigan at Ann Arbor. While there, he was promoted to the rank of captain.
Captain Freeman entered the Air Force Experimental Test Pilot School at Edwards Air Force Base, California, on 3 January 1962 and graduated 17 August 1962. Next he attended the Aerospace Research Pilot School. After completing that course, Freeman remained at the school as an instructor and served as a flight test engineer at Edwards. By this time, Ted Freeman was an experienced pilot with over 3,300 flight hours.
In October 1963, Captain Freeman was selected as a member of NASA’s Astronaut Group Three. The Group was announced to the public on 18 October. Ted Freeman arrived at the Manned Space Flight Center, Houston, Texas, on 15 January 1964. He and his family resided on Blanchmont Lane in Nassau Bay, southeast of Houston.
Freeman was not assigned to a specific flight, but Group Three was intended for the Apollo Program. Ten of the fourteen astronauts went to The Moon.
The T-38A is powered by two General Electric J85-GE-5 turbojet engines. The J85 is a single-shaft axial-flow turbojet engine with an 8-stage compressor section and 2-stage turbine. The J85-GE-5 is rated at 2,680 pounds of thrust (11.921 kilonewtons), and 3,850 pounds (17.126 kilonewtons) with afterburner. It is 108.1 inches (2.746 meters) long, 22.0 inches (0.559 meters) in diameter and weighs 584 pounds (265 kilograms).
The T-38A has a maximum speed of Mach 1.08 (822 miles per hour/1,323 kilometers per hour) at Sea Level, and Mach 1.3 (882 miles per hour/1,419 kilometers per hour) at 30,000 feet (9,144 meters). It has a rate of climb of 33,600 feet per minute (171 meters per second) and a service ceiling of 55,000 feet (16,764 meters). Its range is 1,140 miles (1,835 kilometers).
Between 1959 and 1972, 1,187 T-38s were built at Northrop’s Hawthorne, California, factory. As of 4 September 2018, 546 T-38s remained in the U.S. Air Force active inventory. The U.S. Navy has 10, and as of 30 October 2018, the Federal Aviation Administration reports 29 T-38s registered to NASA.
© 2018, Bryan R. Swopes
30 October 1991: United States Air Force Sikorsky HH-60G Pave Hawk, 88-26110, call sign “Jolly 110,” assigned to the 106th Rescue Wing, New York Air National Guard, headed out into a hurricane that would become known as “The Perfect Storm.” Aboard were Major C. David Ruvola, pilot; Captain Graham Buschor, co-pilot; Staff Sergeant James R. Mioli, flight engineer; and pararescue jumpers Technical Sergeant John Spillane and Technical Sergeant Arden Rick Smith. Their mission was to attempt a rescue 250 miles (400 kilometers) out to sea.
Due to the severity of the storm—a weather buoy located 264 miles (425 kilometers) south of Halifax, Nova Scotia, reported a wave height of 100.7 feet (30.7 meters) on 30 October, the highest ever recorded in that part of the Atlantic Ocean—the Pave Hawk crew was unable to make the rescue and had to return to their base.
Having already refueled from the Lockheed HC-130 Hercules tanker three times during the mission, and with low fuel, a fourth refueling was needed for the helicopter to make it back to the mainland. Because of the the extreme turbulence and lack of visibility, Jolly 110 could not make contact with the refueling drogue trailing behind the airplane.
Major Ruvola made more than 30 attempts, but finally both drogues had been damaged by the severe conditions. With just twenty minutes of fuel remaining, Jolly 110 would have to ditch in the middle of “The Perfect Storm.”
Unable to refuel, Major Ruvola made the decision to ditch the helicopter into the sea while the engines were still running. At 9:30 p.m., the Sikorsky’s number one engine flamed out from fuel starvation. With one engine still operating, Ruvola held the Pave Hawk in a hover over the raging ocean while Buschor, Mioli, Spillane and Smith jumped.
When the number two engine flamed out, Ruvola put the Pave Hawk into a hovering autorotation. Its blades came to a sudden stop when they hit the face of an oncoming wave. Ruvola was about 15 feet (4.6 meters) under water by the time he was able to escape from the sinking helicopter.
The Pave Hawk had gone down 90 miles (145 kilometers) south of Montauk Point in 100-knot (185 kilometers per hour) winds and 80-foot (25 meter) waves. After five hours in the water, four airmen were rescued by USCGC Tamaroa (WMEC-166), a 48-year-old former U.S. Navy fleet tug, operated by the Coast Guard since the end of World War II as a medium endurance cutter.
The search for Rick Smith continued for a week. He was never found.
The Credible Hawks were further upgraded to the MH-60G Pave Hawk standard, which incorporated an inertial navigation system, GPS, and Doppler radar for precision navigation. Low-light television, infrared cameras and night vision systems allowed the MH-60G to operate at night and very low altitude. The Pave Hawk is equipped with an Automatic Flight Control System (AFCS), a very sophisticated autopilot which incorporates automatic hover capability.
Some of the MH-60G Pave Hawks received further upgrades for the special operations mission. Helicopters dedicated to CSAR were redesignated HH-60G. A rescue hoist capable of lifting 600 pounds (272 kilograms) from a 200-foot (60.7 meter) hover is incorporated on the upper right side of the fuselage.
The HH-60G is operated by a crew of two pilots, a flight engineer and gunner. For rescue operations, pararescue jumpers, the famous “P.J.s,” are added to the crew. The helicopter has an overall length of 64 feet, 11 inches (19.787 meters) with rotors turning. The fuselage is 49 feet, 10 inches (15.189 meters) long and 7 feet, 9 inches (2.362 meters) wide. Overall height (rotors turning) is 16 feet, 11 inches (5.156 meters).
The HH-60G has a four-bladed fully-articulated main rotor with elastomeric bearings. It has a diameter of 53 feet, 8 inches (16.358 meters) and turns counterclockwise as seen from above. (The advancing blade is on the helicopter’s right.) The main rotor turns 258 r.p.m., resulting in a blade tip speed of 728 feet per second (222 meters per second). The blades were built with titanium spars and used two different airfoils and a non-linear twist (resulting in a net -16.4°). The outer 20 inches (0.508 meters) were swept aft 20°.
The four-blade bearingless tail rotor assembly is mounted on the right side of a pylon in a tractor configuration. The tail rotor turns clockwise as seen from the helicopter’s left side. (The advancing blade is below the axis of rotation.) The tail rotor has a diameter of 11 feet (3.353 meters) and each blade has a chord of 0.81 feet (0.247 meters) and -18° twist. The tail rotor turns 1,214 r.p.m. and has a tip speed of 699 feet per second (213 meters per second). Because the Black Hawk’s engines are behind the transmission, the aircraft’s center of gravity (c.g.) is also aft. The tail rotor plane is inclined 20° to the left to provide approximately 400 pounds of lift (1.78 kilonewtons) to offset the rearward c.g.
The HH-60G has a cruise speed of 184 miles per hour (296 kilometers per hour) and its maximum speed is 224 miles per hour (361 kilometers per hour). The service ceiling is 14,000 feet (4,267 meters) and maximum range is 373 miles (600 kilometers). The hover ceiling, in ground effect (HIGE) is approximately 10,000 feet (3,048 meters), and out of ground effect (HOGE) is about 6,000 feet (1,830 meters).
Defensive armament consists of two GAU-18A .50-caliber machine guns.
The U.S. Air Force initially purchased 112 HH-60G Pave Hawk helicopters, though as of May 2016, 96 remain in service. Most of these are approaching their design airframe lifetime limit of 7,000 flight hours. Several have passed 10,000 hours. The Air Force will replace them with a new HH-60W, a combat rescue helicopter based on the Sikorsky UH-60M Black Hawk. 21 U.S. Army UH-60Ls were modified to replace HH-60G losses.
The next CSAR helicopter, the HH-60W, based on the Sikorsky UH-60M, made its first flight 17 May 2019. Low-rate production of 10 new Combat Rescue Helicopters was authorized 24 September 2019. The Air Force plans to purchase 113 “Whiskeys.”
On 5 November 2020, the first two HH-60Ws were delivered to Moody AFB, near Valdosta, Georgia.
© 2019, Bryan R. Swopes
30 October 1935: While undergoing evaluation by the U.S. Army Air Corps at Wright Field, northeast of Dayton, Ohio, the Boeing Model 299 Flying Fortress, X13372 ¹—the most technologically sophisticated airplane of its time—took off with Major Ployer P. Hill as pilot.
The largest land airplane built up to that time, the XB-17 “seemed to have defensive machine guns aimed in every direction.” A Seattle Times newspaper reporter, Roland Smith, wrote that it was a “flying fortress.” Boeing copyrighted the name.
Major Hill was the Chief of the Flying Branch, Material Division, at Wright Field. This was his first flight in the airplane. The co-pilot was the Air Corps’ project pilot, Lieutenant Donald Leander Putt. Boeing’s Chief Test Pilot Leslie R. Tower and company mechanic C.W. Benton were also on board, as was Henry Igo of the Pratt & Whitney Aircraft Company.
Immediately after takeoff, the 299 suddenly pitched up, stalled and crashed, then caught fire. Three men, Igo, Benton and Putt, were able to escape from the wreck despite injuries.
First Lieutenant Robert K. Giovannoli, a test pilot assigned to the Material Division at Wright Field, saw the crash and immediately went to help. He made two trips into the burning wreck to rescue Hill and Tower, though later they both died of their injuries.
Lieutenant Giovannoli was awarded the Soldier’s Medal and the Cheney Award for his heroic rescue of two men from the burning wreck of the Boeing Model 299. His citation reads:
General Orders: War Department, General Orders No. 4 (1936)
The official investigation of the crash determined that the prototype bomber’s flight crew had neglected to release the flight control gust locks which are intended to prevent damage to the control surfaces while on the ground. Test Pilot Tower recognized the mistake and tried to release the control locks, but could not reach them from his position in the cockpit.
Experts wondered if the Flying Fortress was too complex an airplane to fly safely. As a direct result of this accident, the “check list” was developed, now required in all aircraft.
After several years of testing, the Model 299 went into production as the B-17 Flying Fortress. By the end of World War II, 12,731 B-17s had been built by Boeing, Douglas and Lockheed Vega.
Hill Air Force Base, north of Salt Lake City, Utah, was named in honor of Major Ployer Peter Hill, U.S. Army Air Corps. The co-pilot, Lieutenant Putt, remained in the service and eventually achieved the rank of Lieutenant General, U.S. Air Force. He died in 1988.
Robert Kinnaird Giovannoli was born at Washington, D.C., 13 March 1904, the second of two sons of Harry Giovannoli, a newspaper editor, and Carrie Kinnaird Giovanolli. His mother died when he was six years old.
Giovannoli graduated from Lexington High School at Lexington, Kentucky, in 1920 and then attended the University of Kentucky, where, in 1925, he earned a Bachelor of Science degree in Mechanical Engineering (B.S.M.E.). He was a member of the Phi Delta Theta (ΦΔΘ) and Tau Beta Phi (ΤΒΦ) fraternities, treasurer of the sophomore class, and president of the American Institute of Electrical Engineers. He was employed by the General Electric Company at Schenectady, New York.
Giovannoli enlisted in the United States Army in 1927. After completing the Air Corps Primary Flying School at Brooks Field, and the Advanced Flying School at Kelly Field, both in San Antonio, Texas, he was commissioned as a second lieutenant in the Air Corps Reserve, 20 October 1928. Lieutenant Giovannoli was called to active duty 8 May 1930. In 1933, he was assigned to a one year Engineering School at Wright Field. He then was assigned to observe naval aircraft operations aboard USS Ranger (CV-4) in the Pacific Ocean.
On 8 March 1936, just a few days after returning from his temporary assignment with the Navy, Lieutenant Giovannoli was killed when the right wing of his Boeing P-26 pursuit, serial number 32-414, came off in flight over Logan Field, near Baltimore, Maryland.
At the time of his death, Lieutenant Giovannoli had not yet been presented his medals.
First Lieutenant Robert Kinnaird Giovannoli, Air Corps, United States Army, was buried at the Bellevue Cemetery, Danville, Kentucky. In 1985, the Robert Kinnaird Giovannoli Scholarship was established to provide scholarships for students in mechanical engineering at the University of Kentucky College of Engineering.
¹ At that time, experimental and restricted category aircraft were prohibited from displaying the letter “N” at the beginning of their registration mark.
© 2018, Bryan R. Swopes
21 October 1959: McDonnell Aircraft Corporation test pilot Gerald (“Zeke”) Huelsbeck was killed while test flying the first prototype YF4H-1 Phantom II, Bureau of Aeronautics serial number (“Bu. No.”) 142259.
In October 1959 the Navy tried, a bit prematurely, for its first world record with the F4H. McDonnell test pilot Gerald “Zeke” Huelsbeck, flying near Edwards AFB, was testing various flight plans for a high-altitude zoom, looking for one to recommend to the Navy test pilot who would fly the record attempt. Huelsbeck was flying the very first F4H prototype when an engine access door blew loose, flames shot through the engine compartment, and the F4H crashed, killing Huelsbeck. (Over the next three years of the F4H-1 test program three aircraft were destroyed and three crew members died, all preparing for record flights.)
—Engineering the F-4 Phantom II: Parts Into Systems by Glenn E. Bugos, Naval Institute Press, Annapolis, Maryland, 1996, Chapter 5 at Page 101.
The flight control system of the YF4H-1 was damaged by the fire and went it out of control at high speed and into a spin. Zeke Huelsbeck did eject but was too low. His parachute did not open. The prototype crashed in an open area near Mt. Pinos in the Los Padres National Forest, Ventura County, California, about 70 miles (113 kilometers) southwest of Edwards.
McDonnell YF4H-1 Bu. No. 142259 was the first prototype Phantom II. It had first been flown by Robert C. Little at Lambert Field, St. Louis, Missouri, 27 May 1958. The Phantom II was designed as a supersonic, high-altitude fleet defense interceptor for the United States Navy. It was a two-place twin engine jet fighter armed with radar- and infrared-homing air-to-air missiles.
Gerald Huelsbeck was born in Wisconsin, 16 April 1928, the third child of Walter Andrew Huelsbeck, a farmer, and Irene M. Voigt Huelsbeck. He attended Carroll College (now, Carroll University) in Waukesha, before joining the United States Navy as a midshipman. He completed flight training at NAS Whiting Field, Florida, and was commissioned as an ensign, 2 June 1950.
In 1950, Ensign Gerald Huelsbeck married Miss Mary Jean Hillary, who had also attended Carroll College. They would have two children.
Huelsbeck was promoted to lieutenant (junior grade), 2 June 1952. Assigned as a fighter pilot during the Korean War, he flew 54 combat missions in the McDonnell F2H Banshee.
While flying in the Navy, Huelsbeck experimented with helmet-mounted cine cameras:
. . . He took a standard gun camera, added a couple of gadgets, and attached it to his helmet, The camera is electrically driven and able to take about two minutes of film with a 50-foot magazine. . . “I spent some time doing ‘hand camera’ work in Korea,” he recalls. “You know, after 54 combat missions, you don’t like to think about crashing while trying to take a picture.”
—The Indianapolis Star, Vol. 53, No. 116, Tuesday, 29 September 1955, Page 4 at Columns 2–4
He was serving with VF-11 at NAS Jacksonville, Florida, when he was selected for the United States Naval Test Pilot School at NAS Patuxent River, Maryland, in July 1953.
“Zeke” Huelsbeck left the Navy in 1955 to accept a position as a test pilot with the McDonnell Aircraft Corporation, St. Louis, Missouri. After several months, he was assigned as an experimental test pilot and project pilot of the F4H program.
At the time of the accident, Zeke Huelsbeck was the most experienced pilot flying the F4H.
Gerald Huelsbeck was 31 years old when he died. He is buried in New Berlin, Wisconsin.
© 2016, Bryan R. Swopes