The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity
The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity
The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity
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248 Lunar Prospec<strong>to</strong>r<br />
Lunar Prospec<strong>to</strong>r<br />
<strong>The</strong> third mission in NASA’s Discovery Program and<br />
the first <strong>to</strong> be competitively selected. Five days after its<br />
1998 launch, Lunar Prospec<strong>to</strong>r entered a polar orbit<br />
aroundtheMoon,101kmhigh,atthestart<strong>of</strong>ayear-long<br />
primary mission. <strong>The</strong> spacecraft was equipped with five<br />
instruments, mounted on three 2.5-m long booms,<br />
including aneutron spectrometer—the first device <strong>of</strong> this<br />
type <strong>to</strong> be carried onboard an interplanetary probe. <strong>The</strong><br />
spectrometer was designed <strong>to</strong> verify the existence <strong>of</strong><br />
water ice at the lunar poles as first suggested by measurements<br />
made by Clementine in 1994. On March 5, 1998,<br />
it was announced that Lunar Prospec<strong>to</strong>r had found further<br />
evidence <strong>to</strong> backup Clementine’s discovery. Lunar<br />
Prospec<strong>to</strong>r also provided a new map that shows the<br />
chemical composition and the magnetic and gravity<br />
fields<strong>of</strong>theMooninunprecedenteddetail.<strong>The</strong>nominal<br />
one-year mission was followed by atwo-year extended<br />
missionduringwhichtheorbitwaslowered<strong>to</strong>analtitude<br />
<strong>of</strong> 50 km and then 10 km <strong>to</strong> obtain higher resolution<br />
measurements. On July 31, 1999, Lunar Prospec<strong>to</strong>r<br />
struck the Moon near the south pole in acontrolled<br />
crash <strong>to</strong> look for further evidence <strong>of</strong> water ice, though<br />
none was found.<br />
Launch<br />
Date: January 6, 1998<br />
Vehicle: Athena II<br />
Site: Cape Canaveral<br />
Size: 1.4 × 1.2 m<br />
Mass: 295 kg (fully fueled); 126 kg (dry)<br />
Lunar Roving Vehicle (LRV)<br />
See <strong>Apollo</strong>.<br />
Lunar-A<br />
A Japanese lunar probe, scheduled for launch in 2003 by<br />
ISAS (Institute <strong>of</strong> Space and Astronautical Science). It<br />
will be the first mission <strong>to</strong> study the Moon’s internal state<br />
using penetra<strong>to</strong>rs. After entering lunar orbit, the spacecraft<br />
will deploy three 13-kg spear-shaped cases, 90 cm<br />
long and 13 cm in diameter. <strong>The</strong>se will be individually<br />
released over a period <strong>of</strong> a month and impact the Moon<br />
at 250 <strong>to</strong> 300 m/s, burrowing 1 <strong>to</strong> 3 m in<strong>to</strong> the surface.<br />
One penetra<strong>to</strong>r will be targeted at the equa<strong>to</strong>rial area <strong>of</strong><br />
the nearside (in the region <strong>of</strong> the <strong>Apollo</strong> 12 and 14 landing<br />
sites), one at the equa<strong>to</strong>rial farside, and one near the<br />
border between the nearside and the farside. <strong>The</strong> penetra<strong>to</strong>rs<br />
are equipped with seismometers and devices <strong>to</strong><br />
measure heat flow, and they will transmit their data <strong>to</strong> the<br />
orbiter as it passes over each penetra<strong>to</strong>r every 15 days.<br />
After deploying the penetra<strong>to</strong>rs, the orbiter will move <strong>to</strong><br />
a 200–300 km near-circular orbit and use its monochromatic<br />
camera <strong>to</strong> image features near the termina<strong>to</strong>r with<br />
a resolution <strong>of</strong> up <strong>to</strong> 30 m.<br />
lunar-orbit rendezvous (LOR)<br />
A spacecraft maneuver involving docking and coupling,<br />
fueling, or transfer in a lunar parking orbit. <strong>The</strong> concept<br />
<strong>of</strong> lunar-orbit rendezvous was first discussed by the Russian<br />
rocket theoretician Yuri Kondratyuk in 1916 and later<br />
by the British scientist H. E. Ross. 284 As a means <strong>of</strong> reaching<br />
the Moon’s surface, it has the advantage that the<br />
lunar landing vehicle can be designed specifically for this<br />
task and be <strong>of</strong> low mass, since all the equipment and supplies<br />
for the return <strong>to</strong> Earth can be left in lunar orbit.<br />
Against this, however, must be set the difficulty and danger<br />
<strong>of</strong> having <strong>to</strong> maneuver and dock two vehicles in lunar<br />
orbit. Despite this drawback, LOR was the technique<br />
chosen <strong>to</strong> convey astronauts <strong>to</strong> and from the Moon in<br />
the <strong>Apollo</strong> program.<br />
Lundin, Bruce T. (1919–)<br />
An American aerospace propulsion engineer. Lundin<br />
earned a B.S. in mechanical engineering from the University<br />
<strong>of</strong> California in 1942 and joined the Lewis Labora<strong>to</strong>ry<br />
(see Glenn Research Center) in 1943. <strong>The</strong>re he<br />
investigated heat transfer and methods <strong>to</strong> improve the<br />
performance <strong>of</strong> World War II aircraft engines. In 1946, he<br />
became chief <strong>of</strong> the jet propulsion research section,<br />
which conducted some <strong>of</strong> America’s early research on<br />
turbojet engines. He became assistant direc<strong>to</strong>r <strong>of</strong> Lewis in<br />
1958 and directed much <strong>of</strong> the center’s efforts in space<br />
propulsion and power generation. Lundin then advanced<br />
through the positions <strong>of</strong> associate direc<strong>to</strong>r for development<br />
at Lewis (1961), managing the development and<br />
operation <strong>of</strong> the Centaur and Agena launch vehicles,<br />
and <strong>of</strong> deputy associate administra<strong>to</strong>r for advanced<br />
research and technology at NASA headquarters (1968),<br />
before becoming acting associate administra<strong>to</strong>r for<br />
advanced research and technology there (1969). Later<br />
that year, he was appointed direc<strong>to</strong>r <strong>of</strong> the Lewis<br />
Research Center, a position he held until his retirement<br />
in 1977.<br />
Lunik<br />
<strong>The</strong> name by which the first three Luna spacecraft were<br />
known in the West.<br />
Lunney, Glynn S. (1936–)<br />
A longtime NASA <strong>of</strong>ficial who trained as an aeronautical<br />
engineer and came <strong>to</strong> the Lewis Labora<strong>to</strong>ry (see Glenn<br />
Research Center) around the time <strong>of</strong> NASA’s creation in<br />
1958 <strong>to</strong> join the Space Task Group developing Project