Tag Archives: Photo Reconnaissance

27 November 1957

Captain Ray C. Schrecengost with "Cin-Min," McDonnell RF-101C Voodoo 56-0156 (Boeing)
Captain Ray W. Schrecengost with “Cin-Min,” McDonnell RF-101C-40-MC Voodoo 56-0166 (Boeing)
Operation Sun Run #2, McDonnell RF-101C Voodoo 56-164. (Greater St. Louis Air and Space Museum via Ron Downey Aviation Archives)
Operation Sun Run #2, McDonnell RF-101C-40-MC Voodoo 56-164. This airplane was written off in South Carolina, 10 October 1960. (Photograph courtesy of Ron Downey via Aviation Archives)
McDonnell RF-101C-40-MC Voodoo 56-0165, Sun-Run, flown for Operation Sun Run, 27 November 1957. (U.S. Air Force)
McDonnell RF-101C-40-MC Voodoo 56-165, Operation Sun-Run #3. This airplane was shot down over North Vietnam, 5 December 1966. The pilot, Lieutenant Colonel Arthur Leonard Warren, 20th Tactical Reconnaissance Squadron, 432nd Tactical Reconnaissance Wing, safely ejected and was in radio contact for two hours after parachuting to the ground. He reported that he was taking fire, and contact was lost. He was listed as Missing in Action. His remains were recovered 17 September 1986 and were buried at the Arlington National Cemetery. (U.S. Air Force)
Operation Sun Run #4, McDonnell RF-101C Voodoo 56-166, flown by Captain Ray C. Schrecengost, U.S. Air Force. (Greater St. Louis Air and Space Museum via Ron Downey)
Operation Sun Run #4, McDonnell RF-101C-40-MC Voodoo 56-166, flown by Captain Ray C. Schrecengost, U.S. Air Force. This airplane is on display at the National Museum of the United States Air Force.  (Photograph courtesy of Ron Downey via Aviation Archives)
Operation Sun-Run #5
Operation Sun-Run #5, McDonnell RF-101C-40-MC Voodoo 56-167. This airplane was written off 24 July 1964. (Photograph courtesy of Ron Downey via Aviation Archives)

27 November 1957: Four U.S. Air Force pilots of the 363rd Tactical Reconnaissance Wing successfully completed Operation Sun Run by establishing three new transcontinental speed records in a McDonnell RF-101C aircraft. The record-breaking mission showcased the speed and range of the RF-101C, an improved version of the first supersonic photo reconnaissance aircraft, the RF-101A.

“Operation Sun Run called for six RF-101C aircraft — two to fly round-trip from Los Angeles to New York and back again, two for the one-way flight from Los Angeles to New York, and two for backups if problems arose with the four primary aircraft. The undertaking required massive coordination of aircraft crews and radar and weather stations from coast to coast.

“Operation Sun Run participants, L–R: Capt. Ray W. Schrecengost, Capt. Robert J. Kilpatrick, Capt. Donald D. Hawkins, Maj. Stanley R. Sebring (18th TRS commanding officer, Operation Sun Run operations officer), Lt. Col. William H. Nelson (9th AF, Operation Sun Run programs officer), Capt. Robert E. Burkhart, Capt. Robert M. Sweet, Lt. Gustav B. Klatt. (U.S. Air Force)”

Six pilots of the 17th and 18th Tactical Reconnaissance Squadrons of the 363rd Tactical Reconnaissance Wing were chosen for Operation Sun Run. Each prepared for the round-trip flight, since they would not know which flight they were assigned until a few days before the operation. All six pilots had extensive experience in photo reconnaissance aircraft, although the RF-101 was relatively new to Tactical Air Command.

“The success of Operation Sun Run also depended on the performance of the newly available KC-135 Stratotanker, the USAF’s first jet tanker. The KC-135’s speed allowed the RF-101s to refuel at an altitude of 35,000 feet and a speed of Mach 0.8. Crews from Strategic Air Command and Air Force Research and Development Command prepared for the 26 refuelings the Operation Sun Run RF-101Cs would require.

“At 6:59 a.m., 27 November 1957, Capt. Ray Schrecengost took off from Ontario International Airport near Los Angeles on the first RF-101C round-trip flight of Operation Sun Run. Next into the air were Capt. Robert Kilpatrick on his one-way flight and Capt. Donald Hawkins, flying back-up. Capt. Hawkins followed until the first refueling was complete, and then flew to March Air Force Base, Calif. At 7:50 a.m., Capt. Robert Sweet took off on the second round-trip flight. Lt. Gustav Klatt followed, beginning his one-way trip. Their backup, Capt. Robert Burkhart, also flew to March Air Force Base after the first successful refueling.

“All four RF-101C pilots easily surpassed the previous speed records and established new ones. The new Los Angeles to New York record was established by Lt. Klatt, at 3 hours, 7 minutes and 43.63 seconds. Capt. Sweet set the round-trip record, at a time of 6 hours, 46 minutes and 36.21 seconds, and the New York to Los Angeles record, at a time of 3 hours, 36 minutes and 32.33 seconds.”

Fact Sheets: Operation Sun Run, National Museum of the United States Air Force

McDonnell RF-101C-40-MC Voodoo 56-166. (U.S. Air Force)
McDonnell RF-101C-40-MC Voodoo 56-166. (U.S. Air Force)

The McDonnell RF-101C Voodoo was an unarmed reconnaissance variant of the F-101C fighter. It was 69 feet, 4 inches (21.133 meters) long with a wingspan of 39 feet, 8 inches (12.090 meters). The height was 18 feet (5.486 meters). Empty weight for the RF-101C was 26,136 pounds (11,855 kilograms), with a maximum takeoff weight of 51,000 pounds (23,133 kilograms).

The RF-101C was powered by two Pratt & Whitney J57-P-13 turbojet engines. The J57 was a two-spool axial-flow turbojet which had a 16-stage compressor (9 low- and 7 high-pressure stages), and a 3-stage turbine (1 high- and 2 low-pressure stages). The J57-P-13 maximum continuous power rating of 8,700 pounds of thrust (38.70 kilonewtons); military power, 10,200 pounds (45.37 kilonewtons) (30-minute limit); and 15,000 pounds (66.72 kilonewtons) with afterburner (5 minute limit). The -P-13 was 3 feet, 4.3 inches (1.024 meters) in diameter, 17 feet, 7.0 inches (5.359 meters) long, and weighed 5,025 pounds (2,279 kilograms).

The aircraft had a maximum speed of  879 knots (1,012 miles per hour/1,629 kilometers per hour) at 35,000 feet (10,668 meters)—Mach 1.53. The service ceiling was 49,600 feet (15,118 meters). The Voodoo could carry up to three drop tanks, giving a total fuel capacity of 3,150 gallons (11,294 liters) and a maximum range of 1,864 nautical miles (2,145 statute miles/3,452 kilometers).

The RF-101C was unarmed. It carried six cameras in its nose. Two Fairchild KA-1s were aimed downward, with four KA-2s facing forward, down and to each side.

Beginning in 1954, McDonnell Aircraft Corporation built 807 F-101 Voodoos. 166 of these were the RF-101C variant. This was the only F-101 Voodoo variant to be used in combat during the Vietnam War. The RF-101C remained in service with the U.S. Air Force until 1979.

Colonel Ray W. Schrecengost's McDonnell RF-101C-40-MC Voodoo, 56-166, was named Cin-Min for his daughters, Cindy and Mindy. The Voodoo is painted in camouflage as it appeared when assigned to the 45th Tactical Reconnaissance Squadron at Tan Son Nhut AB, South Vietnam. It was one of the first aircraft camouflaged for combat in SEA. It is in the collection of the National Museum of the United States Air Force. (U.S. Air Force)
Colonel Ray W. Schrecengost’s McDonnell RF-101C-40-MC Voodoo, 56-166, was named “Cin-Min” for his daughters, Cindy and Mindy. The Voodoo is painted in camouflage as it appeared when assigned to the 45th Tactical Reconnaissance Squadron at Tan Son Nhut AB, South Vietnam. It was one of the first aircraft camouflaged for combat in Southeast Asia. 56-166 is in the collection of the National Museum of the United States Air Force. (U.S. Air Force)
Schrek's Cin-Min on the Sun Run" by William S. Phillips at the National Museum of the United States Air Force, depicts Colonel Schre 's McDonnell RF-101C Voodoo. (U.S. Air Force)
“Schrek’s Cin-Min on the Sun Run” by William S. Phillips, at the National Museum of the United States Air Force, depicts Colonel Schrecengost’s McDonnell RF-101C Voodoo. (U.S. Air Force)

A McDonnell Aircraft Corporation film about Operations Sun Run and Fire Wall is available on YouTube:

© 2018, Bryan R. Swopes

25 November 1940

The prototype de Havilland DH.98 Mosquito, W4050, takes off on its first flight at Hatfield, 25 November 1940. (BAE Systems)

25 November 1940: De Havilland Aircraft Company’s Chief Test Pilot, Geoffrey Raoul de Havilland, Jr., and engineer John Walker, made the first flight of the DH.98 Mosquito prototype, E0234, at Hatfield, Hertfordshire, England. The prototype’s Royal Air Force identification was W4050. The multi-role combat aircraft was constructed primarily of layers of balsa covered with layers of birch, then a layer of doped cotton fabric. It was powered by two Rolls-Royce Merlin V-12 engines.

Sir Geoffrey de Havilland, Jr, with a DH.98 Mosquito, 14 October 1943. (Photo by Reg Speller/Fox Photos/Getty Images 3320005)

The construction materials took advantage of plentiful supplies of wood, and also made workers who were not in the standard metal aircraft industry able to take part.

The prototype was rolled out 19 November 1040, painted overall yellow.

The prototype de Havilland DH.98 Mosquito, E0234, outside the Assembly Building, 19 November 1940. (BAE Systems)

The prototype had a wingspan of 54 feet, 2 inches (16.510 meters), and its gross weight was 19,670 pounds (8,922 kilograms). W4050 was powered by two liquid-cooled, supercharged, 1,648.96-cubic-inch-displacement (27.01 liter) Rolls-Royce Merlin Mk.21 single overhead camshaft (SOHC) 60° V-12 engines, producing 1,460 horsepower at 3,000 r.p.m. at 10,000 feet (3028 meters), with 10 pounds (0.69 Bar) of boost, and driving three-bladed de Havilland Hydromatic propellers through a gear reduction.

The prototype DH.98 Mosquito,now marked W4050, in the field behind Salisbury Hall (where it was designed and built) just before its first flight, 25 November 1940. (HistoryNet)

The DH.98 had been predicted to be 20 miles per hour (32 kilometers per hour) faster than the Supermarine Spitfire, but was actually much faster. In testing, the prototype reached 392 miles per hour (631 kilometers per hour) at 22,000 feet (6,706 meters). Improvements were continuously made, and with 2-stage superchargers, W4050 reached a maximum 437 miles per hour (703 kilometers per hour). The DH.98 prototype had a service ceiling of 34,000 feet (10,363 meters) and range of 2,180 miles (3,500 kilometers).

The production fighter variant, the Mosquito F. Mk.II, was 41 feet, 2 inches (12.548 meters) long with a wingspan of 54 feet, 2 inches (16.510 meters) and height of 15 feet, 3 inches (4.648 meters) in 3-point position. The wings had 1½° incidence with approxmatey 2½° dihedral. The leading edges were swept aft 2½°. The total wing area was 436.7 square feet (40.6 square meters). The fighter’s empty weight was 13,356 pounds (6,058 kilograms) and the maximum takeoff weight was 18,649 pounds (8,459 kilograms). The Mk.II had a total fuel capacity of 553 gallons.

The Mk.II had a cruise speed of 265 miles per hour (426 kilometers per hour) at 15,000 feet (4,572 meters) and maximum speed of 380 miles per hour (612 kilometers per hour) at 21,400 feet (6,523 meters).

Mosquito bomber variants could carry four 500 pound bombs, or two 2,000 pound bombs, but were otherwise unarmed. Fighters were equipped with four Hispano Mk.II 20 mm autocannon and four Browning .303-caliber Mk.II machine guns in the nose.

6,411 DH.98 Mosquitoes were built in England, 1,134 in Canada and 212 in Australia. It was produced in bomber, fighter, night fighter, fighter bomber and photo reconnaissance versions.

The prototype DH.98 Mosquito, W4050, at Hatfield, Hertfordshire. (Royal Air Force)

W4050’s (the prototype’s Royal Air Force identification) fuselage was damaged while taxiing at Boscombe Down, 24 February 1941, and had to be replaced with one intended for a second prototype, W4051. It remained at de Havilland and was used to test different engines, armaments and versions. After a series of tests conducted in December 1943, the prototype Mosquito was permanently grounded. It was used as an instructional airframe and later placed in storage.

In September 1958, W4050 was turned over to the de Havilland Aircraft Heritage Centre. Today, the restored prototype DH.98 Mosquito is at the museum at London Colney, Hertfordshire, England.

The Mosquito prototype with camouflauged upper surfaces as it appeared at Boscombe Down, (de Havilland Aircraft Museum)
The Mosquito prototype with camouflaged upper surfaces as it appeared at Boscombe Down, 1941. (de Havilland Aircraft Museum)

© 2020, Bryan R. Swopes

14 October 1962

This is one of the reconnaissance photographs taken by Major Richard S. Heyser  from his Lockheed U-2, flying at 72,500 feet over Cuba, 14 October 1962. (U.S. Air Force)

14 October 1962: Major Richard Stephen (“Steve”) Heyser, a pilot with the 4028th Strategic Reconnaissance Squadron, 4080th Strategic Reconnaissance Wing, United States Air Force, boarded Item 342, his Top Secret reconnaissance airplane, at Edwards Air Force Base, California. Over the next seven hours he flew from Edwards to McCoy AFB, near Orlando, Florida, landing there at 0920 EST.

Major Richard S. Heyser, U.S. Air Force, with a Lockheed U-2. Major Heyser is wearing a MC-3 capstan-type partial-pressure suit for protection at high altitudes. (U.S. Air Force)
Major Richard S. Heyser, U.S. Air Force, with a Lockheed U-2. Major Heyser is wearing a MC-3 capstan-type partial-pressure suit for protection at high altitudes. (U.S. Air Force)

But first, Steve Heyser and Item 342 flew over the island of Cuba at an altitude of 72,500 feet (22,098 meters). Over the island for just seven minutes, Heyser used the airplane’s cameras to take some of the most important photographs of the Twentieth Century.

Item 342 was a Lockheed U-2F. Designed by Clarence L. (“Kelly”) Johnson at the “Skunk Works,” it was a very high altitude, single-seat, single-engine airplane built for the Central Intelligence Agency. Item 342 carried a U.S. Air Force number on its tail, 66675. This represented its serial number, 56-6675.

It had been built at Burbank, then its sub-assemblies were flown aboard a C-124 Globemaster transport to a secret facility at Groom Lake, Nevada, called “The Ranch,” where it was assembled and flown.

Originally a U-2A, Item 342 was modified to a U-2C, and then to a U-2F, capable of inflight refueling.

Major Heyser had been at Edwards AFB to complete training on the latest configuration when he was assigned to this mission.

A Lockheed U-2A, 56-6708, “Item 375”. (U.S. Air Force)

Major Heyser’s photographs showed Russian SS-4 Sandal intermediate range nuclear-armed missiles being placed in Cuba, with SA-2 Guideline radar-guided surface-to-air anti-aircraft missile sites surrounding the nuclear missile sites.

President John F. Kennedy ordered a blockade of Cuba and demanded that Russia remove the missiles. Premier Nikita Khrushchev refused. The entire U.S. military was brought to readiness for immediate war. This was The Cuban Missile Crisis. World War III was imminent.

(Left to Right) Major Richard S. Heyser, General Curtis E. LeMay and President John F. Kennedy, at the White House, October 1962. (Associated Press)

Richard S. Heyser died 6 October 2008.

© 2017, Bryan R. Swopes

9 October 1943

In this iconic World War II photograph, a Douglas-built B-17F-50-DL Flying Fortress, 42-3352, “Virgin’s Delight,” of the 410th Bomb Squadron, 94th Bombardment Group (Heavy), 8th Air Force, is over the Focke-Wulf Fw 190 fighter factory, Marienburg, East Prussia, 9 October 1943. The aircraft commander was Lieutenant R.E. Le Pore. (U.S. Air Force)

9 October 1943: VIII Bomber Command Mission Number 113 was an attack by nearly 100 American heavy bombers on the Focke-Wulf Flugzeugbau AG aircraft factory at Marienburg, East Prussia (Malbork, Poland), where the Luftwaffe‘s Fw 190 fighter was being built. Early in the war, German fighter production had been dispersed and it was thought that Marienburg was beyond the range of Allied bombers.

The Fw 190 was the most effective of Germany’s fighters. More than 20,000 were built in 16 variants.

A captured Focke-Wulf Fw 190 in flight. (U.S. Air Force)
A captured Focke-Wulf Fw 190 G-3 fighter, DN+FP, W.Nr. 160016, in flight. (U.S. Air Force)
Focke-Wulf Fw 190 G-3 DN+FP, W.Nr. 160016, in flight near Wright Field, Ohio, May 1946. (U.S. Air Force)
Focke-Wulf Fw 190 G-3 DN+FP, W.Nr. 160016, from above and behind. (U.S. Air Force)

100 B-17 Flying Fortress bombers were assigned to the target and 96 of these reached the plant. Between 1253 hours and 1302 hours, the B-17s arrived over the target in five waves at 11,000 to 13,000 feet (3,353 to 3,963 meters). They dropped 217.9 tons (197.7 metric tons) of bombs with a very high degree of accuracy.

During the mission, two B-17s were lost with 13 more damaged. Three airmen were wounded and 21 listed as Missing in Action. The bomber crews claimed 9 Luftwaffe aircraft destroyed and 2 probably destroyed in air-to-air combat. Target assessment estimated that 15 Focke-Wulf Fw 190 fighters were destroyed on the ground.

This strike photo was taken from B-17 42-30353 ("Ten Knights in a Bar Room") of the 95th Bombardment Group (Heavy). (U.S. Air Force)
This strike photo was taken from Boeing B-17F-100-BO Flying Fortress 42-30353 (“Ten Knights in a Bar Room”) of the 95th Bombardment Group (Heavy). (U.S. Air Force)

Casualties among the factory work force were high. Of 669 workers, 114 were killed and 76 injured.

Air Chief Marshal Sir Charles Portal, KCB, DSO, MC, Royal Air Force, described the Marienburg attack as the “. . . most perfect example in history of the accurate distribution of bombs over a target.”

Damage assessment photograph
Reconnaissance photograph taken by a de Havilland DH.98 Mosquito PR flown by Squadron Leader R.A. Lenton and Pilot Officer Heney of No. 540 Squadron, R.A.F., 10 October 1943, showing results of the previous day’s attack. (Royal Air Force)
The target area as it appears today. (Google Maps)
"Instrument workers line up aerial cameras at Benson, Oxfordshire, before installing them in a De Havilland Mosquito PR Mark IX: (left to right) two Type F.24 (14-inch lens) vertical cameras, one F.24 (14-inch lens) oblique camera, two Type F.52 (36-inch lens) 'split pair' vertical cameras." (Imperial War Museum CH-18399)
“Instrument workers line up aerial cameras at Benson, Oxfordshire, before installing them in a De Havilland Mosquito PR Mark IX: (left to right) two Type F.24 (14-inch lens) vertical cameras, one F.24 (14-inch lens) oblique camera, two Type F.52 (36-inch lens) ‘split pair’ vertical cameras.” (Imperial War Museum CH-18399)

© 2017, Bryan R. Swopes

7 July 1946

Hughes XF-11 44-70155 at Culver City, California, 7 July 1946. A Lockheed C-69 Constellation is in the background. (University of Nevada, Las Vegas Libraries)
Hughes XF-11 44-70155 at Culver City, California, 7 July 1946. The prototype Lockheed XC-69 Constellation, 43-10309, now registered NX67900, is in the background. Note the XF-11’s counter-rotating propellers. (University of Nevada, Las Vegas Libraries)

7 July 1946: At the Hughes Aircraft Company’s private airport in Culver City, California, the first of two prototype XF-11 photographic reconnaissance airplanes took of on its first flight. In the cockpit was Howard Robard Hughes, Jr.

Howard Hughes in teh cocpit of the first prototype XF-11, 44-70155, with all propellers turning, at Culver City, California. (University of Nevada, Las Vegas Libraries)
Howard Hughes in the cockpit of the first prototype XF-11, 44-70155, with all propellers turning, at Culver City, California. (University of Nevada, Las Vegas Libraries)

The Hughes XF-11 was designed to be flown by a pilot and a navigator/photographer. Its configuration was similar to the Lockheed P-38 Lightning and Northrop P-61 Black Widow, as well as the earlier Hughes D-2. The prototype was 65 feet, 5 inches (19.939 meters) long with a wingspan of 101 feet, 4 inches (30.886 meters) and height of 23 feet, 2 inches (7.061 meters). The empty weight was 37,100 pounds (16,828.3 kilograms) and maximum takeoff weight was 58,300 pounds (26,444.4 kilograms).

Howard Hughes in teh cockpit of the XF-11 prototype. (Houston Chronicle)

The XF-11 was powered by two air-cooled, supercharged 4,362.49-cubic-inch-displacement (71.49 liter) air-cooled, supercharged Pratt & Whitney R-4360-31 (Wasp Major TSB1-GD) four row, 28-cylinder radial engines. This engine had a compression ratio of 7:1. It had a normal power rating of 2,550 horsepower at 2,550 r.p.m. at 5,000 feet (1,524 meters), and 3,000 horsepower at 2,700 r.p.m. for takeoff. The R-4360-31 was 4 feet, 4.50 inches (1.334 meters) in diameter, 9 feet, 6.25 inches (2.902 meters) long and weighed 3,506 pounds (1,590 kilograms). The engines drove a pair of contra-rotating four-bladed propellers through a 0.381:1 gear reduction.

The planned maximum speed was 450 miles per hour (724 kilometers per hour), service ceiling 44,000 feet (13,411 meters) and planned range was 5,000 miles (8,047 kilometers).

The first prototype Hughes XF-11, 44-70155, taking off from the Hughes Aircraft Company's private airport, Culver City, California. 7 July 1946.(University of Nevada, Las Vegas Libraries)
The first prototype Hughes XF-11, 44-70155, taking off from the Hughes Aircraft Company’s private airport, Culver City, California. 7 July 1946. (University of Nevada, Las Vegas Libraries)

After about an hour of flight, a hydraulic fluid leak caused the rear propeller of the right engine to go into reverse pitch. Rather than shutting the engine down and feathering the propellers to reduce aerodynamic drag, Hughes maintained full power on the right engine but reduced power on the left, attempting to limit adverse yaw to the right side.

Unable to make it back to the Culver City airport, Hughes planned to land at the Los Angeles Country Club. At 7:20 p.m., the airplane crashed into three houses on North Whittier Drive, Beverly Hills, California. The fire destroyed the prototype and one of the houses and heavily damaged the others. Howard Hughes was seriously injured in the crash.

Burning wreckage of Hughes' prototype XF-11 in the yard at 808 N. Whittier Street, Beverly Hills, California. (Unattributed)
Burning wreckage of Hughes’ prototype XF-11 in the yard at 808 N. Whittier Drive, Beverly Hills, California. (Los Angeles Times)
Howard Hughes in an ambulance following the crash of the XF-11. (Los Angles Times)

The investigating board criticized Hughes for not following the flight test plan, staying airborne too long, and deviating from a number of standard test flight protocols. The cause of the actual crash was determined to be pilot error.

The second Hughes XF-11 landing at Culver City. (Los Angeles Times)

A second XF-11 was completed and flew in April 1947, again with Hughes in the cockpit. The project was cancelled however, in favor of the Northrop F-15 Reporter and Boeing RB-50 Superfortress, which were reconnaissance aircraft based on existing combat models already in production.

The second prototype Hughes XF-11, 44-70156, on a test flight near Anacapa Island, off the coast of Southern California, April 1946. (Hughes Aircraft Company)
The second prototype Hughes XF-11, 44-70156, on a test flight near Anacapa Island, off the coast of Southern California, 1947. This airplane does not have counter-rotating propellers. (U.S. Air Force)

© 2019, Bryan R. Swopes