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Lunar Orbiter 5

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Lunar Orbiter 5
NameLunar Orbiter 5
Mission typeLunar orbiter
OperatorNASA / Langley Research Center
COSPAR ID1967-075A
SATCAT02888
Mission duration183 days
SpacecraftLunar Orbiter E
ManufacturerThe Boeing Company
Launch mass1,676 kg (3,695 lb)
Launch dateAugust 1, 1967, 22:33:00 UTC
Launch rocketAtlas SLV-3 Agena D
Launch siteCape Canaveral LC-13
Disposal typeDeorbited
Decay dateJanuary 31, 1968
Orbit referenceSelenocentric orbit
Orbit periapsis194.5 km (120.9 mi)
Orbit apoapsis6,023 km (3,743 mi)
Orbit inclination85 degrees
Orbit period510.08 minutes
Apsisselene

Lunar Orbiter 5 was the final spacecraft in the highly successful Lunar Orbiter program of the NASA. Launched in August 1967, its primary objectives were to conduct high-resolution photographic surveys of key lunar regions, including potential Apollo landing sites, and to gather vital scientific data on the Moon's radiation environment and gravitational field. The mission completed the systematic photographic mapping of the near side and provided the first detailed images of the south polar region, cementing the program's legacy as a critical precursor to crewed lunar exploration.

Mission overview

Authorized by NASA Headquarters, Lunar Orbiter 5 was designed as a hybrid mission, combining the site-confirmation goals of the earlier "A" series orbiters with the broad scientific mapping objectives of the "B" series. Managed by the Langley Research Center, the mission aimed to photograph 36 pre-selected Apollo and Apollo Applications Program sites with a resolution as fine as 2 meters. Additionally, it was tasked with imaging vast swaths of the far side and scientifically intriguing features like the south pole and the Mare Orientale basin. The spacecraft also carried experiments to measure micrometeoroid flux, cosmic radiation, and the lunar gravitational field, contributing to the broader scientific understanding of the Moon.

Spacecraft design

Based on the standardized design developed by The Boeing Company and Eastman Kodak, the spacecraft consisted of a primary structure built around a Mylar-wrapped Magnesium frame. The core photographic system, engineered by Eastman Kodak, featured a dual-lens camera capable of capturing simultaneous wide-angle and high-resolution images on a single strip of 70mm aerographic film. An onboard Bimat transfer process developed the film, which was then scanned by a photomultiplier and transmitted to Earth via a dish antenna. The vehicle was stabilized in flight by a Canopus star tracker and gyroscopes, with trajectory corrections executed by a velocity control engine fueled by hypergolic propellants.

Mission profile and operations

Launched atop an Atlas-Agena D rocket from LC-13 at Cape Canaveral Air Force Station, the spacecraft entered a temporary parking orbit before its Agena upper stage fired for translunar injection. After a 92-hour cruise, Lunar Orbiter 5 performed a critical retrograde burn to achieve an initial elliptical Selenocentric orbit. Over the following weeks, NASA's Deep Space Network stations, including the Goldstone Deep Space Communications Complex, commanded several orbit-lowering maneuvers to reach the optimal photographic orbit. Mission controllers at the Langley Research Center meticulously planned each imaging pass, successfully photographing all primary and secondary targets before concluding the photographic phase on August 18, 1967.

Scientific instruments and experiments

The primary payload was the facsimile camera system, which provided unprecedented imagery. The spacecraft also housed a suite of supporting instruments. A meteoroid detector, mounted on the spacecraft's structure, measured the flux and penetration potential of small particles. Radiation dosimeters monitored the levels of cosmic and trapped radiation encountered in cislunar space and lunar orbit. Furthermore, the mission performed a significant selenodesy experiment by precisely tracking the spacecraft's Doppler shift from Earth, allowing scientists at the MIT and the Jet Propulsion Laboratory to map subtle gravitational anomalies and refine the model of the Moon's gravitational field.

Results and legacy

Lunar Orbiter 5 returned 633 high-resolution and 211 medium-resolution photographs, achieving 100% of its photographic objectives. Its images confirmed the safety of several Apollo landing sites and provided the first clear views of the heavily cratered south polar highlands. The mission's gravitational data significantly advanced the study of mascons, massive concentrations beneath the maria. After completing its tasks, the spacecraft was commanded to impact the lunar surface on January 31, 1968, near the Mare Orientale basin to prevent future interference. The complete photographic atlas produced by the Lunar Orbiter program was instrumental for the success of the Apollo missions and remains a foundational dataset for planetary scientists.

Category:Lunar Orbiter program Category:NASA space probes Category:1967 in spaceflight