Tag Archives: Thor DM-19

19 August 1960

A Fairchild C-119J, 51-8039, recovers a Discovery Satellite Reentry Vehicle. (U.S. Air Force)

19 August 1960: Discoverer XIV was a Keyhole KH-1 reconnaissance satellite of Project CORONA. Mission 9009 was launched by a Thor-Agena A two-stage liquid fueled rocket from Vandenberg Air Force Base, California, at 11:55 p.m. Pacific Standard Time, 18 August 1960 (19:55:00 UTC).¹ The Agena A entered a 186 kilometer × 805 kilometer (115.6 miles × 500.2 miles) elliptical orbit, inclined 79.650°, and the satellite took 1 hour, 34 minutes, 33 seconds to complete each orbit.

After 17 orbits, 7 of which crossed over “denied territory,” the Discoverer Satellite Rentry Vehicle (SRV) was ejected from the Agena A and de-orbited. This ejection took place within 5 seconds of the planned time.

On 19 August, a Fairchild C-119J Flying Boxcar, 51-8037, call sign Pelican 9, of the 6593rd Test Squadron, Hickham Air Force Base, Hawaii, was sent to recover the satellite as it descended through the lower atmosphere by parachute. The air crew sighted the parachute at about 8,000 feet (2,438 meters), 360 miles (580 kilometers) southwest of Hawaii. On their third attempt, they were able to snag the satellite and parachute with recovery equipment deployed under the transport, and then pull it inside. This was the first time that film from a satellite had been recovered.

Corona 1 photographic image of Mys Shmidta Air Field, USSR. This image, taken 18 August 1960, has a resolution of 40 feet x 40 feet ( meters). (National Reconnaissance Office)
Corona 1 photographic image of Mys Shmidta Air Field, Chukotka, Russia, USSR, an intercontinental bomber staging base built in 1954. This image, taken 18 August 1960, has a resolution of 40 feet × 40 feet (12.2 meters × 12.2 meters). The runway is 2,450 meters (8,038 feet) long. (National Reconnaissance Office)

Pelican 9’s pilot, Captain Harold Ellis Mitchell (22 June 1925–14 February 2013) was awarded the Distinguished Flying Cross. The other members of the crew received the Air Medal.

Flight Crew of Fairchild C-119J 51-8037, circa 1960. Front row, left to right: Captain Harold Ellis Mitchell, Captain David Torgerson, 1st Lieutenant Robert Counts, Staff Sergeant Arthur Hurst, Airman Second Class Thierry Franc; back row: Technical Sergeant Louis Bannick, Staff Sergeant Algaene Harmon, A2C George Donohou, A2C Lester Beale and A2C Daniel Hill. (U.S. Air Force)

The Agena A remained in orbit until 16 September 1960.

Mission 9009 photographed 1.5 million square miles (3.9 million square kilometers) of Soviet and Eastern Europe countries.

The mission summary reads:

     Mission 9009 was accomplished on 18 August 1960. It consists of eight north-south passes over the USSR and includes portions of China, the Satellites and Yugoslavia (see accompanying coverage map).

     Approximately 25 percent of the coverage is cloud free, with light-scattered to heavy clouds covering the remainder of the photography. The PI quality of the unobscured coverage ranges from good to very good.

     The scale of the photography is estimated to range from 1:300,000 to 1:450,000.

     Major items of intelligence significance covered by Mission 9009 incluse the Kapsutin Yar Missile lTest Range (KYMTR), the western portion of the presumed 1,050 nm impact area of the KYMTR, 20 newly identified hexadic SA-2 surface to air missile sites and six possible SA-2 sites under construction, the Sarova Nuclear Weapons Research and Development Center, several new airfields, and numerous urban complexes.

CORONA: America’s First Satellite Program, Kevin C. Ruffner, Editor, and CIA History Staff. Center of the Study of Intelligence, Central Intelligence Agency, Washington, D.C., 1995, at  Page 120

The mission report contains a lengthy list of airfields and military installations of intelligence interest to the United States.

Project CORONA had been proposed by the Advanced Research Projects Agency (ARPA) and was managed by the Central Intelligence Agency and the United States Air Force. The Discoverer program was publicly explained as an Earth sciences research project, with some carrying live monkeys, but was actually a Central Intelligence Agency program for the reconnaissance of the Soviet Union and China.

Lockheed Missiles and Space Company at Sunnyvale, California, was the prime contractor, while Fairchild Camera and Instrument Co. was responsible for the KH-1 camera system. General Electric built the Satellite Reentry Vehicle (SRV).

Lockheed RM-81 Agena A. (U.S. Air Force via Drew ex Machina)
Internal Arrangement of Corona spacecraft. (Drew ex Machina)

The Discoverer reconnaissance payload was carried into orbit by a Lockheed RM-81 Agena A. This was a liquid-fueled rocket used as a second stage for the Thor first stage booster. The Agena A was 15.51 feet (4.73 meters) long and 4.98 feet (1.52 meters) in diameter. It had an empty weight of 1,951 pounds (885 kilograms) and maximum weight of 8,350 pounds (3,790 kilograms).

Early Agena As were powered by a single Bell 8001 (XLR81-BA-3) rocket engine which had originally been developed as a Rocket Assisted Takeoff (RATO) unit for the Convair B-58A Hustler Mach 3 strategic bomber. This was upgraded to the Bell 8048 (XLR81-BA-5) for most Agena As. This engine weighed 279 pounds (126.6 kilograms). Burning Nitric Acid and UDMH, it produced 15,589 pounds of thrust (69.343 kilonewtons). The engine had a burn time of 120 seconds. The engine nozzle was gimballed for pitch and yaw control.

Bell Model 8048 (XLR81-BA-5) rocket engine in the collection of the National Museum of the United States Air Force. (U.S Air Force)

The Agena A nose cone carried a Fairchild Camera and Instrument Co. KH-1 panoramic camera system. It used 20 pounds (kilograms) of 70 mm film. The camera used an ITEK Corporation HYAK B lens with an f/5.0 aperture and focal length of 61 centimeters. Its ground resolution was 11.7 meters. The camera transferred the film to the reentry vehicle.

Resolution was not as good as could be obtained by a Lockheed U-2 reconnaissance plane, but the Discoverer XIV was able to cover areas that the U-2 never reached.

The Agena A orbiter also had a TOD-4 navigation payload.

Internal arrangement of Discoverer photographic system. (Drew ex Machina)

When it was time to eject the SRV, the Agena A pitched down 60°. The SRV was spin-stabilized by small rockets, and then a retro rocket fired to decelerate it into a descent trajectory.

Fairchild C-119J-FA Flying Boxcar 51-8037 at the National Air and Space Museum, Wright Patterson Air Force Base, Ohio. (U.S. Air Force)

51-8037 had been built as a C-119F Packet “Flying Boxcar” and delivered to the U.S. Air Force on 2 June 1953. It was converted to a C-119J at the Birmingham Modification Center in Birmingham, Alabama, during October 1956. From September 1958 to November 1959, it was further modified specifically to recover space capsules. The satellite recovery airplane is in the collection of the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio.

The C-119F Flying Boxcar is a large twin-engine transport aircraft with a distinctive twin boom configuration. It has a high wing and retractable tricycle landing gear. It normally carried a flight crew of five, consisting of two pilots, a navigator, radio operator and crew chief. It could carry 42 troops, or a maximum of 62 troops for emergency evacuation. Alternatively, it could transport 35 litter patients and 4 attendants. The airplane is 86.5 feet (26.365 meters) long with a wingspan of 109.3 feet (33.315 meters) and overall height of 26.5 feet (8.077 meters. It has a total wing area of 1,447.2 square feet (134.45 square meters). The C-119F has an empty weight of 40,118 pounds (18,197 kilograms), and takeoff weight of 77,000 pounds (34,927 kilograms). The cargo payload is 20,650 pounds (9,367 kilograms).

The C-119F was powered by two air-cooled, supercharged and fuel injected, 3,347.66 cubic-inch displacement (543.858 liter) Wright 868TC18DB1 Cyclone 18 (R-3350-85) two-row, 18-cylinder radial engines. These engines were also known as the Duplex-Cyclone. They had a compression ratio of 6.7:1 and required 115/145 octane aviation gasoline. The Normal Power rating was 2,650 horsepower at 2,650 r.p.m. (continuous); Takeoff Power rating, 3,500 horsepower at 2,900 horsepower at 2,900 r.p.m. at Sea Level (5 minute limit); and Military Power rating of 3,500 horsepower at 2,900 r.p.m. at 4,500 feet (1,372 meters) with a 30 minute limit. This decreased to 2,550 horsepower at 15,400 feet (4,694 meters), and retained the 30 minute limit. The R-3350-85 had a length of 90.80 inches (2.306 meters), diameter of 56.59 inches (1.437 meters), and weighed 3,472 pounds (1,575 kilograms. It used a 0.4375:1 gear reduction. 2,395 of these engines were produced between September 1951 and 1954.

This airplane had a maximum speed of 265 knots (305 miles per hour/491 kilometers per hour) at 17,900 feet (5,456 meters) at maximum power. Its cruise speed was 248 knots (285 miles per hour/459 kilometers per hour) at 5,000 feet (1,524 meters).

The C-119F could takeoff after a ground run of 3,875 feet (1,181 meters), and had a rate of climb of 795 feet per minute (4.04 meters per second) at Sea Level with Normal Power at its takeoff weight of 77,000 pounds (34,927 kilograms). At a combat weight of 49,360 pounds (22,389 kilograms) and using maximum power, it could climb at 2,320 feet per minute (11.8 meters per second). Its service ceiling was 26,600 feet (8,108 meters) at maximum power.

With a maximum fuel capacity of 2,590 gallons (9,804 liters) and maximum payload, the C-119F had a combat range of 1,462 nautical miles (1,682 statute miles/2,708 kilometers) at 158 knots (182 miles per hour/292 kilometers per hour).

Fairchild produced 1,183 C-119s between 1949 and 1955.

¹ Launch windows were scheduled to avoid the passage of Southern Pacific Railroad passenger trains which ran along the coast at Vandenberg, to prevent the spacecraft being seen by the public. Sometime only a few minutes were available between passing trains.

© 2024, Bryan R. Swopes

17 August 1958

Thor-Able 127 being prepared for launch at the Cape Canaveral Air Force Station. (U.S. Air Force)

17 August 1958: In what was the first attempt to launch a spacecraft beyond Earth orbit, Thor-Able 1 (Missile Number 127) was to place a small instrumented satellite in orbit around the Moon. Called Pioneer,¹ the satellite carried a television camera, a micrometeorite detector and a magnetometer.

The mission was carried out by the U.S. Air Force Ballistic Missile Division and the Advanced Research Projects Agency (ARPA).

The Thor-Able lifted off from Launch Complex 17A at the Cape Canaveral Air Force Station, Florida, at 12:28:00 UTC, 4 minutes behind schedule.

73.6 seconds into the flight, at an altitude of 9.9 miles (16 kilometers), the first stage of the rocket exploded. Telemetry from the upper stages continued and was tracked until impact in the Atlantic Ocean.

An investigation found the cause of the explosion to be a turbopump failure. It was determined that a bearing in the pump’s gearbox seized, halting the flow of liquid oxygen.

The Thor Able was a two-stage orbital launch vehicle which was developed from the Douglas Aircraft Company’s SM-75 Thor intermediate-range ballistic missile.

Designated Thor DM-19, the first stage was 60.43 feet (18.42 meters) long and 8 feet (2.44 meters) in diameter. Fully fueled, the first stage had a gross weight of 108,770 pounds (49,337 kilograms). It was powered by a Rocketdyne LR-79-7 engine which burned liquid oxygen and RP-1 (a highly-refined kerosene rocket fuel) and produced 170,565 pounds of thrust (758.711 kilonewtons). This stage had a burn time of 2 minutes, 45 seconds.

The second stage was an Aerojet General Corporation-built Able, a second stage for the U.S. Navy’s Vanguard rocket. It was 21 feet, 6.6 inches (6.57 meters) long with a maximum diameter of 2 feet, 9 inches (0.84 meters), and had a gross weight of 5,000 pounds (2,268 kilograms). It used an Aerojet AJ10-101 rocket engine which burned a hypergolic mixture of nitric acid and UDMH. The second stage produced 7,711 pounds of thrust (34.300 kilonewtons) and burned for 1 minutes, 55 seconds.

Thor-Able second stage being prepared to mount to the Thor 127 first stage. (Drew ex Machina)

The Altair X248 third stage was developed by the Alleghany Ballistics Laboratory for the U.S. Navy’s Vanguard rocket. It was 4 feet, 11 inches (1.499 meters) long, 2 feet, 7 inches (0.787 meters) in diameter, and weighed 505 pounds (229 kilograms). It was powered by a solid fuel rocket engine producing 2,300 pounds (10.231 kilonewtons) of thrust. Its burn time was 38 seconds.

Thor-Able 127 lifts off from Launch Complex 17A, 17 August 1958. (NASA)

The first Pioneer space probe is today designated Pioneer 0. It was built by the Ramo-Wooldridge Corporation’s Space Technologies Laboratory (STL) in Redondo Beach, California.

The lunar probe was the fourth stage  of the Thor-Able launch vehicle. It was 74 centimeters (2 feet, 5.13 inches) in diameter, 76 centimeters (2 feet, 5.9 inches) long, and weighed 38.1 kilograms (83.996 pounds). The probe’s external shell was constructed of metal and fiberglass. It carried 11.3 kilograms (24.9 pounds) of instruments designed to measure magnetic fields, radiation and micrometeorites. It also carried an infrared camera system intended to obtain close-up images of The Moon’s surface. Pioneer 0 was spin-stabilized, turning 108 r.p.m.

The probe was equipped with a Thiokol TX-8-6 solid rocket engine to decelerate it for entry into lunar orbit. The rocket engine was the main structural component of the probe. There were 8 vernier rockets to correct its trajectory.

Space Technologies Laboratory Pioneer lunar orbiter. (STL/Drew ex Machina)

The Thiokol TX-8 was produced at the U.S. Army’s Longhorn Army Ammunition Plant near Karnack, Texas. It was designed to power the GAR-1 Falcon radar-homing air-to-air guided missile (later designated AIM-4 Falcon). The rocket motor weighed 11 kilograms (24.3 pounds).

Arrangement of equipment within the Pioneer lunar orbiter. (Drew ex Machina)

¹ Pioneer 0 was also known as Able 1.

© 2024, Bryan R. Swopes

12 August 1960, 09:39:43 UTC

The Thor Delta launch vehicle at Launch Complex 17A, Cape Canaveral Air Force Station. The spherical capsule containing the Echo 1A is visible at the top of the Altair solid fuel third stage. (NASA)

12 August 1960: At 5:39:43 a.m., Eastern Daylight Savings Time, the Echo 1A experimental passive communications satellite was launched from LC-17A at Cape Canaveral Air Force Station, Florida. The launch vehicle was a Thor-Delta three stage rocket. It entered a nearly circular 944 mile × 1,048 mile orbit (1,519 × 1,687 kilometers). The orbital period was 118.3 minutes.

The satellite was a 100 foot diameter (30.48 meter) Mylar polyester balloon with a reflective surface. The material was just 0.0127 millimeters thick. The mass of the satellite was 66 kilograms (145.5 pounds). In orbit, the balloon envelope was kept inflated by gas from evaporating liquid. It had been constructed by the G.T. Schjeldahl Company, Northfield, Minnesota. This was the second Echo satellite. The first had failed to reach orbit when launched 13 March 1960.

Later the same day, a microwave transmission from the Jet Propulsion Laboratory, Pasadena, California, was reflected off the Echo 1A satellite and received at the Bell Laboratories, Homdel, New York.

According to NASA, “The success of Echo 1A proved that microwave transmission to and from satellites in space was understood and demonstrated the promise of communications satellites. The vehicle also provided data for the calculation of atmospheric density and solar pressure due to its large area-to-mass ratio. Echo 1A was visible to the unaided eye over most of the Earth (brighter than most stars) and was probably seen by more people than any other man-made object in space.”

Echo 1A remained in Earth orbit until 24 May 1968.

An Echo satellite undergoing static inflation tests inside a blimp hangar at Weeksville NAS, North Carolina. The vehicle, which shows scale, is a 1959 Plymouth Suburban 4-door station wagon. (NASA)

The Delta was a three-stage expendable launch vehicle which was developed from the Douglas Aircraft Company’s SM-75 Thor intermediate-range ballistic missile.

Designated Thor DM-19, the first stage was 60.43 feet (18.42 meters) long and 8 feet (2.44 meters) in diameter. Fully fueled, the first stage had a gross weight of 108,770 pounds (49,337 kilograms). It was powered by a Rocketdyne LR-79-7 engine which burned liquid oxygen and RP-1 (a highly-refined kerosene rocket fuel) and produced 170,565 pounds of thrust (758.711 kilonewtons). This stage had a burn time of 2 minutes, 45 seconds.

The second stage was an Aerojet General Corporation-built Delta 104. It was 19 feet, 3 inches (5.88 meters) long with a maximum diameter of 4 feet, 6 inches (1.40 meters). The second stage had a gross weight of 9,859 pounds (4,472 kilograms). It used an Aerojet AJ10-104 rocket engine which burned a hypergolic  mixture of nitric acid and UDMH. The second stage produced 7,890 pounds of thrust (35.096 kilonewtons) and burned for 4 minutes, 38 seconds.

The third stage was an Alleghany Ballistics Laboratory Altair 1. It was 6 feet long, 1 foot, 6 inches in diameter and had a gross weight of 524 pounds (238 kilograms). This stage used a solid-fuel Thiokol X-248 rocket engine, producing 2,799 pounds of thrust (12.451 kilonewtons). Its burn time was 4 minutes, 16 seconds.

© 2016, Bryan R. Swopes