Each of the six Apollo landers touched down at unique sites on the lunar surface. Aside from the Apollo 12 landing site located 180 meters from the Surveyor III lander, plume impingement effects on ground hardware during the landings were not a problem. The planned return to the Moon requires numerous landings at the same site. Since the top few centimeters of lunar soil are loosely packed regolith, plume impingement from the lander will eject the granular material at high velocities. A picture shows what the astronauts viewed from the window of the Apollo 14 lander. There was tremendous dust excavation beneath the vehicle. With high-vacuum conditions on the Moon (10 (exp -14) to 10 (exp -12) torr), motion of all particles is completely bal...
The soil mechanics investigation was conducted to obtain information relating to the landing interac...
A technique to estimate mass erosion rate of surface soil during landing of the Apollo Lunar Module ...
Abstract. Plume impingement effects from the descent and ascent engine firings of the Lunar Lander w...
The Constellation Project's planned return to the moon requires numerous landings at the same site. ...
The rocket exhaust of spacecraft landing on the Moon causes a number of observable effects that need...
The Apollo 12 lunar module (LM) landing near the Surveyor 1lI spacecraft at the end of 1969 has rema...
textWhen a lander approaches a dusty surface, the plume from the descent engine impinges on the grou...
Several physical mechanisms are involved in excavating granular materials beneath a vertical jet of ...
This paper is a summary compilation of work accomplished over the past decade at NASA’s Kennedy Spac...
During the Apollo missions it became apparent that lunar dust was a significant hazard. Problems inc...
The President's Vision for Space Exploration calls for the return of human exploration of the Moon. ...
Plume generation from descent rockets impinges on the lunar landing site regolith, rendering sites h...
Characterizing dust plumes on the moon's surface during a rocket landing is imperative to the succes...
Humanity is on course to return to the surface of the Moon within the next decade, with plans and as...
In preparation for the Apollo program, Leonard Roberts developed a remarkable analytical theory that...
The soil mechanics investigation was conducted to obtain information relating to the landing interac...
A technique to estimate mass erosion rate of surface soil during landing of the Apollo Lunar Module ...
Abstract. Plume impingement effects from the descent and ascent engine firings of the Lunar Lander w...
The Constellation Project's planned return to the moon requires numerous landings at the same site. ...
The rocket exhaust of spacecraft landing on the Moon causes a number of observable effects that need...
The Apollo 12 lunar module (LM) landing near the Surveyor 1lI spacecraft at the end of 1969 has rema...
textWhen a lander approaches a dusty surface, the plume from the descent engine impinges on the grou...
Several physical mechanisms are involved in excavating granular materials beneath a vertical jet of ...
This paper is a summary compilation of work accomplished over the past decade at NASA’s Kennedy Spac...
During the Apollo missions it became apparent that lunar dust was a significant hazard. Problems inc...
The President's Vision for Space Exploration calls for the return of human exploration of the Moon. ...
Plume generation from descent rockets impinges on the lunar landing site regolith, rendering sites h...
Characterizing dust plumes on the moon's surface during a rocket landing is imperative to the succes...
Humanity is on course to return to the surface of the Moon within the next decade, with plans and as...
In preparation for the Apollo program, Leonard Roberts developed a remarkable analytical theory that...
The soil mechanics investigation was conducted to obtain information relating to the landing interac...
A technique to estimate mass erosion rate of surface soil during landing of the Apollo Lunar Module ...
Abstract. Plume impingement effects from the descent and ascent engine firings of the Lunar Lander w...