Digitally enhanced image of the surface of Venus captured by the Venera 9 lander, 22 October 1975. (NASA)Mosaic of images of the surface of Venus captured by the Venera 9 lander, 22 October 1975. The rocks are estimated to be 30–40 centimeters across. (NASA)
22 October 1975, 05:13 UTC: The lander from the Soviet space probe Venera 9 touched down on the surface of the planet Venus, at approximately 32° south latitude, 291° east longitude.
Venera 9 lander. (NASA)
The images and other data was transmitted to an orbiting section of Venera 9 for relay to Earth. The lander sent signals for approximately 53 minutes before the orbiter traveled out of range.
Venera 9 orbiter. (NASA)
Venera 9 had been launched from the Baikonur Cosmodrome aboard a Proton-K rocket, 8 June 1975. The space probe weighed 4,936 kilograms (10,882 pounds).
Once in orbit around Venus, the spacecraft separated into the orbiter and lander. As the lander descended to the surface, data was collected about the planet’s atmosphere. A 40-kilometer (25-mile) deep layer of clouds was studied. The cloud bases were about 35–40 kilometers (22–25 miles) above the surface. The clouds contained hydrochloric and hydrofluoric acid, bromine and iodine.
At the planet’s surface the atmospheric pressure was 90 times that of Earth’s. The temperature was measured at 485 °C. (905 °F.).
Pioneer 1 is readied for launch aboard a Thor Able I at Launch Complex 17A, Cape Canaveral Air Force Station. (NASA Image Number 73-H-787)
11 October 1958: At 08:42:13 UTC (3:42:13 a.m., Eastern Standard Time), Able 2 (later renamed Pioneer 1) was launched from Launch Complex 17A at the Cape Canaveral Air Force Station on the east coast of Florida., on a mission to orbit The Moon. The launch vehicle was Thor Number 130, DM-1812-6. The mission was carried out by the U.S. Air Force Ballistic Missile Division, the Advanced Research Projects Agency (ARPA), and the newly established National Aeronautics and Space Administration (NASA).
The Thor second stage shut down approximately 10 seconds earlier than planned. An accelerometer had cut off the engine because of an incorrect valve setting. As a result, the space probe did not achieve sufficient velocity to escape Earth’s gravity. It reached a maximum altitude of 71,303 miles (114,751 kilometers) at 11:42 UTC.
An attempt to insert the space probe into a 79,970 × 20,000 mile (128,699 × 32,187 kilometers) orbit failed. The internal temperatures were too cold for the stage’s batteries to ignite the solid fuel rocket engine. 43 hours after launch, Able 2 reentered the atmosphere at 03:46 UTC, 13 October 1958, over the South Pacific Ocean.
The Able 2 space probe is today designated Pioneer 1. It was built by the Ramo-Wooldridge Corporation’s Space Technology Laboratory (STL) in Redondo Beach, California.
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.
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.
Arrangement of equipment with the Pioneer lunar orbiter. (Drew ex Machina)A Pioneer lunar orbiter attached to the third stage of the Thor-Able launch vehicle. (U.S. Air Force)
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 1 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. 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).
7 October 1959: An E-2A space probe, Luna 3, was launched by the Union of Soviet Socialist Republics at 00:43:39.7 UTC, 4 October 1959, from the Tyuratam Launch Complex (now known as the Baikonur Cosmodrome). The launch vehicle was a 3-stage 8K72 rocket, a variant of the R7 Semyorka two-stage intercontinental ballistic missile. Luna 3 was approximately cylindrical, 130 centimeters (4 feet, 3.2 inches) long, with a diameter of 120 centimeters (3 feet, 11.2 inches). It weighed 278.5 kilograms (614 pounds).
At 1416 UTC, 6 October, the probe made its closest approach as it passed over the lunar south pole at 6,200 kilometers (3,852 miles) and continued around the far side of The Moon in an highly eccentric orbit. For 40 minutes, between 0330 and 0410 UTC, 7 October, cameras aboard Luna 3 took a series of images of the surface. These photographs, taken at a distance of 63,500 to 66,700 kilometers (39,457 to 41,445 miles), were the first photos ever taken of The Moon’s far side. Exposed film from the cameras was processed on board, then transmitted to Earth as television signals.
The orbit of Luna 3 was highly eccentric with a 15 day period. It came as close as 40,638 kilometers and as far as 460,755 kilometers (25,251 miles to 286,300 miles) from The Moon. Contact was lost 22 October 1959. It is believed to have reentered the Earth’s atmosphere after April 1960.
Image of the far side of The Moon captured by Luna 3, 7 October 1959.
Earth and The Moon, photographed by Voyager 1, 18 September 1977. (NASA)
“This picture of the Earth and Moon in a single frame, the first of its kind ever taken by a spacecraft, was recorded September 18, 1977, by NASA’s Voyager 1 when it was 7.25 million miles (11.66 million kilometers) from Earth. The moon is at the top of the picture and beyond the Earth as viewed by Voyager. In the picture are eastern Asia, the western Pacific Ocean and part of the Arctic. Voyager 1 was directly above Mt. Everest (on the night side of the planet at 25 degrees north latitude) when the picture was taken. The photo was made from three images taken through color filters, then processed by the Image Processing Lab at Jet Propulsion Laboratory (JPL). Because the Earth is many times brighter than the Moon, the Moon was artificially brightened by a factor of three relative to the Earth by computer enhancement so that both bodies would show clearly in the prints. Voyager 1 was launched September 5, 1977 and Voyager 2 on August 20, 1977. JPL is responsible for the Voyager mission.”
The Voyager 1 interplanetary space probe was launched from Launch Complex 41, Kennedy Space Center, Cape Canaveral, Florida, at 12:56:00 UTC, 5 September 1977. (NASA)
