January 10 


10 January 1946

Project Diana radar antenna at Fort Monmouth, New Jersey, USA.
Credit: InfoAge Science History Learning Center and Museum

On January 10, 1946, a team of military and civilian personnel at Camp Evans, Fort Monmouth, New Jersey, USA, reflected the first radar signals off the Moon using a specially modified SCR-270/1 radar. The signals took 2.5 seconds to travel to the Moon and back to the Earth. This achievement, Project Diana, marked the beginning of radar astronomy and space communications. The effort resolved doubts about whether electromagnetic waves suitable for long-range communication and radar could penetrate the Earth’s ionosphere. It was the first documented experiment in radar astronomy and in actively probing another celestial body, and was the dawn of the space age.

   Following the end of World War II, Col. John H. DeWitt Jr. (1906–1999), Director of the Evans Signal Laboratory at Camp Evans (part of Fort Monmouth), in Wall Township, New Jersey, was directed by the Pentagon to determine whether the ionosphere could be penetrated by radar, in order to detect and track enemy ballistic missiles that might enter the ionosphere. He decided to address this charge by attempting to bounce radar waves off the Moon. For this task he assembled a team of engineers that included Chief Scientist E. King Stodola (1914–1992), Herbert Kauffman (1914–1980), Jacob Mofenson (1914–1969), and Harold Webb (1909–1989). Input from other Camp Evans units was sought on various issues, including most notably the mathematician Walter McAfee (1914–1995), who made the required mathematical calculations. 

Project Diana staff from left: Jacob Mofenson, Harold D. Webb, John H. DeWitt, Jr., E. King Stodola, and Herbert P. Kauffman.
Credit: US Army Communications Electronics Museum

   The reflective array antenna consisted of 64 half-wavelength dipoles in an 8x8 array in front of a flat reflective screen, and had a gain of 24 dB and a main lobe beamwidth of about 15°. It was driven by a 50 kW modified SCR-271 radar set that produced quarter-second pulses. The whole assembly was mounted atop a 100-foot reinforced tower. The signals had a frequency of 115.5 MHz, the peak power was 15 kW. The echoes took about 2.5 seconds to return. The receiver had to compensate for the Doppler shift in frequency of the reflected signal due to the Moon's orbital motion relative to the Earth's surface, which was different each day, so this motion had to be carefully calculated for each trial. The antenna could be rotated in azimuth only so the experiment could only be done at moonrise and moonset as the moon passed through the antenna's horizontal beam.

   The first successful echo detection came on January 10, 1946 at 11:58 am local time by Harold Webb and Herbert Kauffman. The experiment was concluded at 12:09 pm, when the Moon moved out of the radar's range. The experiment was repeated daily over the next three days and on eight additional occasions during the month.

    Although the possibility of reflecting radar signals off the Moon had been discussed in the scientific literature, there are no prior documented similar achievements. Zoltán Bay (1900–1992) and a Hungarian team achieved a similar result on February 6, 1946. Because their receiver did not have the sensitivity required, and their antenna did not have the gain needed to directly detect the reflected signal, they used an accumulating coulometer to acquire a 30 fold increase in the signal to noise ratio, producing a signal, post processing, 4% above the noise floor.

   Demonstrating that signals could travel from the Earth to the Moon and back was proof of concept for the idea of what is known as Earth-Moon-Earth (EME), or “moonbounce” communication. Following the success of the project, the US Navy set out to explore the implications and applications of this form of communication - the idea of a reliable, secure EME scheme. The system in its completed state began seeing use in 1960 and was expanded to accommodate ship-to-shore transmissions. In the later 1960s it became obsolete due to the advent of artificial satellites in orbit to serve the same purpose.

Oscilloscope display showing the Project Diana radar signal. The large pulse on the left is the transmitted signal, the small pulse on the right is the return signal from the Moon. The horizontal axis is time, but is calibrated in miles. It can be seen that the measured range is 238,000 mi (383,000 km), the distance from the Earth to the Moon. Credit: Radio News Magazine

© 2026, Andrew Mirecki


10 January 1968

Engineering model, S-10, of the Surveyor lunar lander at the Smithsonian's National Air and Space Museum. It was reconfigured to represent a flight model of Surveyor III or later, since it was the first to have a scoop and claw surface sampler. Credit: Mark Avino. Smithsonian's National Air and Space Museum

Surveyor VII, the last of the series of Surveyor lunar probes, successfully landed on the Moon near the outer rim of the Tycho crater on January 10, 1968, at 01:05:36.3 UT. at 40.9812º S, 11.5127º W (as determined from Lunar Reconnaissance Orbiter images). The lander had returned a total of about 21,000 pictures of itself and its surroundings and studied the chemical composition of the lunar surface. Last contact with the lander took place on February 21, 1968.

The specific objectives for this mission were to: 
(1) perform a lunar soft landing (in a highland area well removed from the maria to provide a type of terrain photography and lunar sample significantly different from those of other Surveyor missions); 
(2) obtain postlanding TV pictures; 
(3) determine the relative abundances of chemical elements; 
(4) manipulate the lunar material; 
(5) obtain touchdown dynamics data; and, 
(6) obtain thermal and radar reflectivity data. Surveyor 7 was the only Surveyor craft to land in the lunar highland region.

A Surveyor VII landing site panorama, using newly digitized data. 
Credit: NASA/JPL-Caltech/University of Arizona Lunar and Planetary Laboratory/Gary Rennilson

   During the first lunar day, 20,993 television pictures were obtained. An additional 45 pictures were obtained during the second lunar day. The alpha-scattering instrument, after completing its background count in the intermediate position, failed to deploy the remainder of the distance to the lunar surface. The surface sampler was then brought in to action and, by means of a series of intricate maneuvers, was able to force the alpha-scattering instrument to the surface. The surface sampler was later used to pick up the alpha-scattering instrument after the first chemical analysis had been completed and to move it to two other locations for additional analyses. These delicate operations demonstrated the versatility of the surface sampler as a remote manipulation device and the precision with which its operations can be controlled from the Earth.

    Approximately 66 hours of alpha-scattering data were obtained during the first lunar day on three samples: the undisturbed lunar surface, a lunar rock, and an area dug up by the surface sampler. An additional 34 hours of data were obtained on the third sample during the second lunar day. The surface sampler dug a number of trenches and conducted static and dynamic bearing­ strengths of the lunar material. The performance of the instrument and its controllers was outstanding.

   In addition to acquiring a wide variety of lunar surface data, Surveyor VII also obtained pictures of the Earth and performed star surveys. Laser beams from the Earth were success­fully detected by the spacecraft's television camera in a special test of laser-pointing techniques.  

   Post sunset operations were conducted for 15 hours after local sunset at the end of the first lunar day at 06 :06 GMT on January 25, 1968. During these operations, additional Earth and star pictures were obtained, as were observations of the solar corona out to 50 solar radii. Operation of the spacecraft was terminated at 14:12 GMT on January 26, 1968, 80 hours after sunset. Second lunar-day operations began at 19:01 GMT on February 12, 1968, and continued until 00:24 GMT on February 21, 1968.

The scoop of the surface sampler, shown in the middle of the photograph, being used to help deploy the sensor head of the Alpha Scattering Experiment (on the left) on January 12, 1968.  
Credit: NASA (from Andrew LePage. Surveyor 7: The Mission to Tycho. Drew Ex Machina)

The Surveyor photograph of the partially sunlit Earth, taken by Surveyor VII at 09:06 UT on January 20, 1968, shows two narrow laser beams sent to the Moon from the Kitt Peak National Observatory, near Tucson, Ariz., and the Table Mountain Observatory, near Los Angeles. The blue-green argon-ion laser beams seen within the white circle on the photograph each contained only about 1 watt of power. This was an engineering test to gain experience for the Apollo laser-ranging retroreflector experiment.
Credit: NASA (from Andrew LePage. Surveyor 7: The Mission to Tycho. Drew Ex Machina)


Surveyor VII, sitting on the ejecta blanket of Tycho Crater. Lunar Reconnaissance Orbiter image NAC M175355093L, image width is 500 m. Inset is zoomed 4x. Credit: NASA/GSFC/Arizona State University


© 2026, Andrew Mirecki


10 January 1969

Preflight preparations of Venera 5 or Venera 6. Credit: NPO Lavochkin

Venera 6 spacecraft was launched from Baikonur on January 10, 1969, at 05:51:52 UTC, on a Molniya 8K78M launch vehicle. Its lander capsule entered the Venusian atmosphere on May 17, 1969.
 
   Venera 5 and Venera 6 spacecraft were of identical design and launched 5 days apart in January 1969. The spacecraft were designed to make in-situ measurements as they descended through the Venusian atmosphere. Measurements included temperature, pressure, and composition. 
 
   Venera 5 spacecraft was very similar to Venera 4 although it was of a stronger design. It comprised a bus with a mass of 1130 kg which held the descent probe. The probe was spherical with a mass of 405 kg and was designed for decelerations as high as 450-g. Venera 5 and 6 were designed with smaller parachutes (15 square meters) than Venera 4 to allow them to fall faster so as to get lower in the atmosphere while still operational. The top of the probe would be ejected to deploy the parachute and expose the instruments to the atmosphere. The probe carried a radio altimeter, two resistance thermometers, an aneroid barometer, eleven gas analyzer cartridges, an ionization densitometer, and photoelectric sensors. The probe also carried a medallion bearing the coat of arms of the U.S.S.R. and a bas-relief of V.I. Lenin to the night side of Venus.

   The bus was essentially identical to the Venera 4 bus. It was 3.5 meter high and powered by 2.5 square meters of solar panel "wings" with a span of 4 meters. A 2.3 meter diameter high-gain parabolic dish antenna was mounted on the cylinder facing opposite the solar panels and a cone-shaped omni-directional antenna was mounted at the end of one of the solar panels. There was a large rocket for mid-course maneuvering, and a set of smaller thrusters, with Sun, Earth, and star sensors, for attitude control. Communications from the probe were achieved by two 1 bit/sec transmitters in the DM waveband. The bus held energetic particle detectors, charged particle traps, and an ultraviolet photometer.  
 
© 2026, Andrew Mirecki


10 January 1975

Soyuz 17 crew: A. Gubarev (right) and G. Grechko

Soyuz 17 spacecraft, with cosmonauts Aleksei A. Gubarev (1931–2015) and Georgy M. Grechko (1931–2017), was launched on January 10, 1975. It was the first of two long-duration missions to the Salyut 4 space station. The cosmonauts returned to Earth after 29 days on February 9, 1975.

Mission data:

Mission name: Soyuz 17
Crew: Aleksei A. Gubarev (Алексе́й Алекса́ндрович Гу́барев) – Commander
           Georgy M. Grechko (Георгий Михайлович Гречко) – Flight engineer
Spacecraft: Soyuz 7K-T No. 38
Launch vehicle: Soyuz 11A511 (No. Kh15000-022)
Launch site: NIIP-5, LC1
Launch date and time: 10 January 1975, 21:43:37 UTC
Landing date and time: 9 February 1975, 11:03:22 UTC
Landing site: 110 kilometres NE of Tselinograd, Kazakhstan
Flight duration: 29 d 13 h 19 min 45 s

Aleksei Gubarev onboard Salyut 4. Credit: SpaceFacts.de

Salyut 4 with Soyuz spacecraft diagram


© 2026, Andrew Mirecki


10 January 1978

Soyuz 27 crew: V. Dzhanibekov (left) and O. Makarov

Soyuz 27 spacecraft, with cosmonauts Vladimir A. Dzhanibekov (born 1942) and Oleg G. Makarov (1933–2003), was launched to the Salyut 6 space station on January 10, 1978. The main goal of the mission was to swap Soyuz craft with the orbiting crew, in so doing freeing a docking port for a forthcoming supply Progress spacecraft. The cosmonauts returned to Earth on January 16, 1978, in the Soyuz 26 capsule.

Mission data:

Mission name: Soyuz 27
Crew: Vladimir A. Dzhanibekov (Владимир Александрович Джанибеков) – Commander
           Oleg G. Makarov (Олег Григорьевич Макаров) – Flight engineer
Spacecraft: Soyuz 7K-T No. 44
Launch vehicle: Soyuz-U (No. D 15000-106)
Launch site: NIIP-5, LC1
Launch date and time: 10 January 1978, 12:26:00 UTC
Landing date and time: 16 January 1978, 11:24:58 UTC (in Soyuz 26)
Landing site: 265 kilometres W of Tselinograd, Kazakhstan
Flight duration: 5 d 22 h 58 min 58 s

Vladimir Dzhanibekov onboard Salyut 6. Credit: SpaceFacts.de

Diagram of the Salyut 6 station


© 2026, Andrew Mirecki






























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