Finalmente trovato quello che cercavo:
11:
Apollo 11 was a Type G mission, a piloted lunar landing demonstration. The primary objective of the Apollo program was to perform a piloted lunar landing and return safely to Earth.
12:
Apollo 12 was a Type H mission, a precision piloted lunar landing demonstration and systematic lunar exploration. It was the second successful human landing on the Moon.
The primary objectives were:
to perform selenological inspection, survey, and sampling in a mare area;
to deploy the Apollo Lunar Surface Experiments Package (ALSEP);
to develop techniques for a point landing capability;
to further develop human capability to work in the lunar environment; and
to obtain photographs of candidate exploration sites.
13:Apollo 13 was planned as a Type H mission, a precision piloted lunar landing demonstration and systematic lunar exploration. It was, however, aborted during translunar flight because of the loss of all the oxygen stored in two tanks in the service module.
The primary objectives were:
to perform selenological inspection, survey, and sampling of materials in a preselected region of the Fra Mauro formation;
to deploy and activate an Apollo lunar surface experiments package;
to further develop human capability to work in the lunar environment; and
to obtain photographs of candidate exploration sites.
14:
Apollo 14 was a Type H mission, a precision piloted lunar landing demonstration and systematic lunar exploration. It was the third successful lunar landing.
The primary objectives were:
to perform selenological inspection, survey, and sampling of materials in a preselected region of the Fra Mauro formation;
to deploy and activate the Apollo lunar surface experiments package;
to develop human capability of working in the lunar environment;
to obtain photographs of candidate exploration sites.
Although the primary mission objectives for Apollo 14 were the same as those of Apollo 13, provisions were made for returning a significantly greater quantity of lunar material and scientific data than had been possible previously. An innovation that allowed an increase in the range of lunar surface exploration and in the amount of material collected was the provision of a collapsible two-wheeled cart, the modular equipment transporter (MET), for carrying tools, cameras, a portable magnetometer, and lunar samples.
15:
The chosen landing site was an area near the foot of the Montes Apenninus (Apennine Mountains) and adjacent to Hadley Rille.
The primary objectives for Apollo 15 were:
to perform selenological inspection, survey, and sampling of materials and surface features in a preselected area of the Hadley-Apennine region;
to emplace and activate surface experiments;
to evaluate the capability of the Apollo equipment to provide extended lunar surface stay time, increased extravehicular operations, and surface mobility; and
to conduct inflight experiments and photographic tasks from lunar orbit.
16:
Apollo 16 was the second Type J mission, an extensive scientific investigation of the Moon from the lunar surface and from lunar orbit. The vehicles and payload were similar to those of Apollo 15.
The primary objectives were:
to perform selenological inspection, survey, and sampling of materials and surface features in a preselected area of the Descartes region;
to emplace and activate surface experiments; and
to conduct inflight experiments and photographic tasks.
17:
Apollo 17 was the third Type J mission, an extensive scientific investigation of the Moon on the lunar surface and from lunar orbit. Although the spacecraft and launch vehicle were similar to those for Apollo 15 and 16, some experiments were unique to this mission. It was also the final piloted lunar landing mission of the Apollo program.
The primary objectives were:
to perform selenological inspection, survey, and sampling of materials and surface features in a preselected area of the Taurus-Littrow region;
to emplace and activate surface experiments; and
to conduct inflight experiments and photographic tasks.
The targeted landing site, Taurus-Littrow, was selected because of the certainty of acquiring highlands material, the potential for superior orbital coverage, and for better use of the LRV.
http://history.nasa.gov/SP-4029/Apollo_00g_Table_of_Contents.htm
