From Wikipedia, the free encyclopedia
Lunar Orbiter 4 was designed to take advantage
of the fact that the three previous Lunar 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 purposes 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.
Instruments
| Lunar Photographic Studies : |
Evaluation of Apollo and Surveyor landing sites |
Meteoroid
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 |
External
links