The Apollo program included several seismometers that were left on the lunar surface and provided data on the Moon’s seismic activity. However, these seismometers were all placed on the lunar near side at Apollo landing sites and were limited by the sensitivity of then-current electronics. The Far-side Seismic Suite (FSS), currently in development and intended to be delivered to the lunar surface on the upcoming CP-12 Commercial Lunar Payload Services (CLPS) mission, plans to be an example of the next generation of lunar seismometers, extending the Apollo seismic data set with data collected on the lunar far side and with modern instrumentation.FSS’ goal is to answer several open scientific questions: 1) What is the deep lunar structure of the moon, and how does it influence the difference between near side and far side seismicity; 2) How has the lunar crust been affected by the development of an impact melt basin; and 3) What is the current micrometeorite impact rate? In order to do so, FSS is designed to accommodate seismometers with heritage from the NASA InSight mission to Mars and last for several months on the lunar surface. Because FSS’ host lander is not designed to last past the first lunar daylight period after landing, FSS includes independent power, communications, and thermal control systems that allow FSS to not only survive but also collect data throughout multiple lunar nights.In this paper, we will discuss the science goals of FSS and its expected performance, provide an overview of the technical implementation of a quasi-independent lunar payload, discuss its similarities to and differences from InSight, and describe the unique opportunities and challenges of operating within NASA’s CLPS framework.

measure lunar surface temperatures, and a seismometer designed with sensitivity high enough to detect the impact of a 2.3 kg (5 lb) meteorite on the opposite A Moon landing or lunar landing is the arrival of a crewed or robotic spacecraft on the Moon. The first human-made object to touch the Moon was Luna 2 in 1959, and the first crewed mission to land on the Moon was Apollo 11 in 1969. There were six crewed landings between 1969 and 1972 and numerous uncrewed landings. All crewed missions to the Moon were conducted by the Apollo program, with the last Soviet… This payload sphere contained six silver-cadmium batteries to power a fifty-milliwatt radio transmitter, a temperature sensitive voltage controlled oscillator to measure lunar surface temperatures, and a seismometer designed with sensitivity high enough to detect the impact of a 2.3 kg (5 lb) meteorite on the opposite side of the Moon. Weight was distributed in the payload sphere so it would rotate in its liquid blanket to place the seismometer into an upright and operational position no matter what the final resting orientation of the external landing sphere. After landing, plugs were to be opened allowing the freon to evaporate and the payload sphere to settle into upright contact with the landing sphere. The batteries were sized to allow up to three months of operation for the payload sphere. Various mission constraints limited the landing site to Oceanus Procellarum on the lunar equator, which the lander ideally would reach 66 hours after launch. No cameras were carried by the Ranger landers, and no pictures were to be captured from the lunar surface during the mission. Instead, the 3.1 metres (10 ft) Ranger Block II mother ship carried a 200-scan-line television camera to capture images during the free-fall descent to the lunar surface. The camera was designed to transmit a picture every 10 seconds. Seconds before impact, at 5 and 0.6 kilometres (3.11 and 0.37 mi) above the lunar surface, the Ranger mother ships took pictures (which may be viewed here). Other instruments gathering data before the mother ship crashed onto the Moon were a gamma ray spectrometer to measure overall lunar chemical composition and a radar altimeter. The radar altimeter was to give a signal ejecting the landing capsule and its solid-fueled braking rocket overboard from the Block II mother ship. The braking rocket was to slow and the landing sphere to a dead stop at 330 metres (1,080 ft) above the surface and separate, allowing the landing sphere to free fall once more and hit the surface. On Ranger 3, failure of the Atlas guidance system and a software error aboard the Agena upper stage combined to put the spacecraft on a course that would miss the Moon. Attempts to salvage lunar photography during a flyby of the Moon were thwarted by in-flight failure of the onboard flight computer. This was probably because of prior heat sterilization of the spacecraft by keeping it above the boiling point of water for 24 hours on the ground, to protect the Moon from being contaminated by Earth organisms. Ranger 3 later began orbiting the Sun, called heliocentric orbit. Heat sterilization was also blamed for subsequent in-flight failures of the spacecraft computer on Ranger 4 and the power subsystem on Ranger 5. Only Ranger 4 reached the Moon in an uncontrolled crash impact on the far side of the Moon. Block III probes replaced the Block II landing capsule and its retrorocket with a heavier, more capable television system to support landing site selection for upcoming Apollo crewed Moon landing missions. Six cameras were designed to take thousands of high-altitude photographs in the final twenty-minute period before crashing on the lunar surface. Camera resolution was 1,132 scan lines, far higher than the 525 lines found in a typical U.S. 1964 home television. Soviet leader Nikita Khrushchev said in October 1963 the USSR was "not at present planning flight by cosmonauts to the Moon," while insisting that the Soviets had not dropped out of the race. Only after another year did the USSR fully commit itself to a Moon-landing attempt, which ultimately failed. At the same time, Kennedy had suggested various joint programs, including a possible Moon landing by Soviet and U.S. astronauts and the development of better weather-monitoring satellites, eventually resulting in the Apollo-Soyuz mission. Khrushchev, sensing an attempt by Kennedy to steal Russian space technology, rejected the idea at first: if the USSR went to the Moon, it would go alone. Though Khrushchev was eventually warming up to the idea, the realization of a joint Moon landing was choked by Kennedy's assassination. Sergey Korolev, the Soviet space program's chief designer, had started promoting his Soyuz craft and the N1 launcher rocket that would have the capability of carrying out a human Moon landing. Khrushchev directed Korolev's design bureau to arrange further space firsts by modifying the existing Vostok technology, while a second team started building a completely new launcher and craft, the Proton booster and the Zond, for a human cislunar flight in 1966. In 1964 the new Soviet leadership gave Korolev the backing for a Moon landing effort and brought all crewed projects under his direction. With Korolev's death and the failure of the first Soyuz flight in 1967, coordination of the Soviet Moon landing program quickly unraveled. The Soviets built a landing craft and selected cosmonauts for a mission that would have placed Alexei Leonov on the Moon's surface, but with the successive launch failures of the N1 booster in 1969, plans for a crewed landing suffered first delay and then cancellation. A program of automated return vehicles was begun, in the hope of being the first to return lunar rocks. This had several failures. It eventually succeeded with Luna 16 in 1970. But this had little impact, because the Apollo 11 and Apollo 12 lunar landings and rock returns had already taken place by then.

Abstract Technology advancement in modern planetary exploration has extended extraterrestrial geological science by sending rovers on challenging, possibly risky but highly scientific-valuable ventures, such as ascending towards the crater walls, traversing steep slopes of sand dunes and travelling through the lava tube. On the 41st lunar day, the first lunar farside prospector, the Yutu-2 rover, carried out an exciting expedition towards a scientifically interesting fin-shaped rock for spectral investigation, taking a high risk of wheel skidding and lateral slippage along a narrow and uneven passage. The rover successfully achieved new findings by extending its locomotion margin on perilous peaks, while its safety was maintained on the basis of ingenious exploration strategies and digital twin-based performance analysis. Surface morphology analysis of the fin-shaped rock indicates that it has suffered certain degrees of impacts. The further in situ spectral investigations suggest that the target rock is composed of Fe/Mg-rich low-Ca pyroxene, thus inferred to belongs to the Zhinyu crater ejecta, rather than those of the Finsen crater. Engineering locomotive data of the rover was used for comprehensive lunar regolith property identification, presenting the first shear parameter range of the farside regolith and an initial estimation on its lateral property in the extraterrestrial environment. The estimated internal friction angle is within 21.5°-42.0° and the associated cohes Technology enabled science: investigation of a fin-shaped rock by the Yutu-2 rover on the lunar farside | Research Square Cite Share Download PDF Article Technology enabled science: investigation of a fin-shaped rock by the Yutu-2 rover on the lunar farside Liang Ding, Ruyi Zhou, Tianyi Yu, Huaiguang Yang, Ximing He, Haibo Gao, and 22 more This is a preprint; it has not been peer reviewed by a journal. On the 41st lunar day, the first lunar farside prospector, the Yutu-2 rover, carried out an exciting expedition towards a scientifically interesting fin-shaped rock for spectral investigation, taking a high risk of wheel skidding and lateral slippage along a narrow and uneven passage. The rover successfully achieved new findings by extending its locomotion margin on perilous peaks, while its safety was maintained on the basis of ingenious exploration strategies and digital twin-based performance analysis. Surface morphology analysis of the fin-shaped rock indicates that it has suffered certain degrees of impacts. The further in situ spectral investigations suggest that the target rock is composed of Fe/Mg-rich low-Ca pyroxene, thus inferred to belongs to the Zhinyu crater ejecta, rather than those of the Finsen crater. Engineering locomotive data of the rover was used for comprehensive lunar regolith property identification, presenting the first shear parameter range of the farside regolith and an initial estimation on its lateral property in the extraterrestrial environment. The estimated internal friction angle is within 21.5°-42.0° and the associated cohesion is 520-3154 Pa, which suggests that the lunar regolith at Chang’E-4 site had similar shear characteristics to samples measured by direct shear approach on the Apollo 12 mission, but relatively larger cohesion than the counterpart investigated on most of nearside lunar missions. This study demonstrates a paradigm of the in-depth integration of science and technology in space exploration, where planetary science is enabled by engineering support, and new demands of scientific exploration in turn generate motivation for the improvement of technology.