To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.

Lunar Orbiter 4

From Wikipedia, the free encyclopedia

Lunar Orbiter 4
Lunar Orbiter 4 image of Moon with Earth.jpg
Image taken by Lunar Orbiter 4, showing the Moon with a crescent Earth in the background. Enhanced by LOIRP.
Mission typeLunar orbiter
COSPAR ID1967-041A
SATCAT no.2772
Mission duration180 days
Spacecraft properties
ManufacturerLangley Research Center
Launch mass385.6 kilograms (850 lb)
Start of mission
Launch dateMay 4, 1967, 22:25:00 (1967-05-04UTC22:25Z) UTC[1]
RocketAtlas SLV-3 Agena-D
Launch siteCape Canaveral LC-13
End of mission
Last contactJuly 17, 1967 (1967-07-18)[2]
Decay dateOctober 6, 1967[3]
Orbital parameters
Reference systemSelenocentric
Semi-major axis6,152.5 kilometers (3,823.0 mi)
Periselene altitude4,449 kilometers (2,764 mi)
Aposelene altitude7,856 kilometers (4,881 mi)
Inclination85.5 degrees
Period721 minutes
EpochMarch 7, 1967, 20:00:00 UTC[4]
Lunar orbiter
Orbital insertionMay 8, 1967, 21:54 UTC

Lunar Orbiter 4 was a robotic U.S. spacecraft, part of the Lunar Orbiter Program, designed to orbit the Moon, after the three previous orbiters had completed the required needs for Apollo mapping and site selection. It was given a more general objective, to "perform a broad systematic photographic survey of lunar surface features in order to increase the scientific knowledge of their nature, origin, and processes, and to serve as a basis for selecting sites for more detailed scientific study by subsequent orbital and landing missions". It was also equipped to collect selenodetic, radiation intensity, and micrometeoroid impact data. The spacecraft was placed in a cislunar trajectory and injected into an elliptical near polar high lunar orbit for data acquisition. The orbit was 2,706 by 6,111 kilometres (1,681 mi × 3,797 mi) with an inclination of 85.5 degrees and a period of 12 hours.

After initial photography on May 11, 1967 problems started occurring with the camera's thermal door, which was not responding well to commands to open and close. Fear that the door could become stuck in the closed position covering the camera lenses led to a decision to leave the door open. This required extra attitude control maneuvers on each orbit to prevent light leakage into the camera which would ruin the film. On May 13 it was discovered that light leakage was damaging some of the film, and the door was tested and partially closed. Some fogging of the lens was then suspected due to condensation resulting from the lower temperatures. Changes in the attitude raised the temperature of the camera and generally eliminated the fogging. Continuing problems with the readout drive mechanism starting and stopping beginning on May 20 resulted in a decision to terminate the photographic portion of the mission on May 26. Despite problems with the readout drive the entire film was read and transmitted. The spacecraft acquired photographic data from May 11 to 26, 1967, and readout occurred through June 1, 1967. The orbit was then lowered to gather orbital data for the upcoming Lunar Orbiter 5 mission.

A total of 419 high-resolution and 127 medium-resolution frames were acquired, covering 99% of the Moon's near side at resolutions from 58 to 134 metres (190 to 440 ft). Accurate data was acquired from all other experiments throughout the mission. Radiation data showed increased dosages due to solar particle events producing low energy protons. The spacecraft was used for tracking until it struck the lunar surface due to the natural decay of the orbit no later than October 31, 1967, between 22–30 degrees W longitude.

Spacecraft orbit and photographic coverage on the near side (left) and far side (right)
Spacecraft orbit and photographic coverage on the near side (left) and far side (right)
Lunar Photographic Studies : Evaluation of Apollo and Surveyor landing sites
Detectors :
Detection of micrometeoroids in the lunar environment
Caesium Iodide Dosimeters : Radiation environment en route to and near the Moon
Selenodesy : Gravitational field and physical properties of the Moon

YouTube Encyclopedic

  • 1/5
    5 191
    3 376
    23 934
    100 153
  • Lunar Photography: "Assignment: Shoot the Moon" 1967 NASA; Ranger, Surveyor, Lunar Orbiter
  • Lunar Orbiter: A Spacecraft to Advance Lunar Exploration 1965 NASA-Boeing
  • Mariner IV: "Eight Months to Mars" 1965 NASA-USIA; Alfred Bester; John Fitch
  • Lunar Reconnaissance Orbiter Apollo Landing Site Images 2011 NASA Goddard
  • NASA | Exploration Mission-1 – Pushing Farther Into Deep Space


See also


  1. ^
  2. ^
  3. ^
  4. ^ "NASA - NSSDCA - Spacecraft - Trajectory Details". Retrieved 2018-05-02.

External links

This page was last edited on 13 May 2021, at 04:42
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.