Instrument Host Information
IDENTIFIER urn:nasa:pds:context:instrument_host:spacecraft.a17a::1.2
NAME APOLLO 17 LUNAR SURFACE EXPERIMENTS PACKAGE
TYPE Spacecraft
DESCRIPTION
Instrument Host Overview
  ========================
    The Apollo 17 Lunar Surface Experiments Package (ALSEP) was carried
    on the Apollo 17 lunar module spacecraft.  It contained scientific
    experiments to be deployed and left on the lunar surface, and other
    scientific and sample collection apparatus. The ALSEP central
    station, located at 20.1921 North latitude, 30.7649 East longitude
    [DAVIES&COLVIN2000], was turned on at 02:53 UT on 12 December 1972
    and shut down along with the other ALSEP stations on 30 September
    1977. For more information, see the ALSEP termination report by
    Bates, et al. (1979) [BATESETAL1979].
 
    ALSEP consisted of a set of scientific instruments emplaced near the
    Apollo 17 landing site by the astronauts. The instruments were arrayed
    around a central station which supplied power to run the instruments
    and communications so data collected by the experiments could be
    relayed to Earth. The central station was a 25 kg box with a stowed
    volume of 34,800 cubic cm. Thermal control was achieved by passive
    elements (insulation, reflectors, thermal coatings) as well as power
    dissipation resistors and heaters. Communications with Earth were
    achieved through a 58 cm long, 3.8 cm diameter modified axial-helical
    antenna mounted on top of the central station and pointed towards Earth
    by the astronauts. Transmitters, receivers, data processors and
    multiplexers were housed within the central station. Data collected
    from the instruments were converted into a telemetry format and
    transmitted to Earth. The ALSEP system and instruments were controlled
    by commands from Earth. The uplink frequency for all Apollo mission
    ALSEP's was 2119 MHz, the downlink frequency for the Apollo 17 ALSEP
    was 2275.5 MHz.
 
    A radioisotope thermoelectric generator (RTG, SNAP-27 model) produced
    the power to run the ALSEP operations. The generator consisted of a 46
    cm high central cylinder and eight radiating rectangular fins with a
    total tip-to-tip diameter of 40 cm. The central cylinder had a thinner
    concentric inner cylinder inside, and the two cylinders were attached
    along their surfaces by 442 spring-loaded lead-telluride thermoelectric
    couples mounted radially along the length of the cylinders. The
    generator assembly had a total mass of 17 kg. The power source was an
    approximately 4 kg fuel capsule in the shape of a long rod which
    contained plutonium-238 and was placed in the inner cylinder of the RTG
    by the astronauts on deployment. Plutonium-238 decays with a half-life
    of 89.6 years and produces heat. This heat would conduct from the inner
    cylinder to the outer via the thermocouples which would convert the
    heat directly to electrical power. Excess heat on the outer cylinder
    would be radiated to space by the fins. The RTG produced approximately
    70 W DC at 16 V. (63.5 W after one year.) The electricity was routed
    through a cable to a power conditioning unit and a power distribution
    unit in the central station to supply the correct voltage and power to
    each instrument.
 
 
    ALSEP Scientific Instruments
    ----------------------------
      All ALSEP instruments were deployed on the surface by the astronauts
      and attached to the central station by cables. The Apollo 17 ALSEP
      instruments consisted of: (1) a heat flow experiment, designed to
      measure the rate of heat loss from the lunar interior and the thermal
      properties of lunar material; (2) a lunar surface gravimeter,
      designed to measure the lunar surface gravity and its temporal
      variations at a selected point on the surface; (3) a lunar mass
      spectrometer, designed to measure the composition of the tenuous
      lunar atmosphere; (4) a lunar seismic profiling experiment, to study
      the physical properties of lunar surface and subsurface materials and
      the structure of the local near-surface layers; and (5) a lunar
      ejecta and meteorites experiment, designed to measure the speed,
      direction, energy, and momentum of cosmic dust particles and lunar
      ejecta. The central station, located at 20.1921 North latitude,
      30.7649 East longitude, was turned on at 02:53 UT on 12 December 1972
      and shut down along with the other ALSEP stations on 30 September
      1977. See the Apollo 17 preliminary science report (1973)
      [APOLLO17A1973] for more information about the ALSEP experiments.
 
 
    This instrument description was provided by the NASA National Space
    Science Data Center.
NAIF INSTRUMENT IDENTIFIER A17A
SERIAL NUMBER
REFERENCES Apollo 17 Preliminary Science Report, NASA SP-330, published by NASA, Washington, D.C., 1973.

Bates, J.R., W.W. Lauderdale, and H. Kernaghan, ALSEP termination report, NASA Reference Publication Series, NASA-RP-1036, 162 pages, published by NASA, Washington, D.C., 1979.

Davies, M.E., and T.R. Colvin, Lunar coordinates in the regions of the Apollo landers, Journal of Geophysical Research, Volume 105, Issue E8, pages 20,227-20,280, 2000, doi:10.1029/1999JE001165.