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Geodesy in the Year 2000 (1990) / Chapter Skim
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Lasers for Geodesy in the Year 2000
Pages 91-99

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From page 91...
... In 1983 NASA organized a meeting called the Airlie House Conference (Walter, 1984) to discuss the scientific requirements for future space geodetic systems, including laser ranging.
From page 92...
... At the present time flashlamps used in laser ranging systems have effective lifetimes on the order of 106 shots -- months of actual operation or days of continuous operation, while the potential for diode pumping is on the order-of 109 shots -- decades of actual operation or years of continuous operation. This development of long lifetime lasers makes spaceborne systems viable.
From page 93...
... This may cause pulse rates to increase from their present 5 to 10 pulses per second to the order of 1000 pulses per second, and for return pulses to be averaged to produce an accurate measurement. The design of the laser array and precise knowledge of the array's position with respect to the center of mass of the spacecraft could become a limiting factor in the development of increasingly accurate laser ranging systems.
From page 94...
... In the mapping mode, the system would obtain 300 meter spots that would be interpolated to provide a 1-2 kilometer global lunar topographic grid appropriate for geodetic and geophysical studies and regional characterization of all major terrain types. In the high resolution mode, LOLA would obtain 30 meter spots to be used for localscale geological profiling.
From page 95...
... from the EOS platform or a similar system; and (3) laser altimetry providing topographic information of the Earth and Moon, and possibly the planets, at the 30 cm vertical precision level with decameter horizontal resolution.
From page 96...
... L Bufton, Lunar Observer Laser Altimeter: Geoscience Applications, Lunar Planet.
From page 97...
... 97 Table 1: The Laser Transmitter 1987 1 color flash lamp pumping flash lamp efficiency 1% - 2% laser lifetimes: 106 shots pulse length: 100 x 10-~2 sees Table 2: Accuracy (best systems) Pulse rate Laser Energy Pulse length Data communication Automation 2000 2 colors diode pumping Ground-Based Laser System 1987 1 cm (excl.
From page 98...
... 0.1 milliradians 40 pps 18 cm Table 4: Characteristics of the EOS and lunar laser altimeters EOS Orbital altitude Frequency Pulsewidth Energy/pulse Receiver telescope diameter Spot size Lunar 800 km 1064 rim 100 ps 120 mj 50 cm 80, 160 m 100 km 1064 rim 3 us 2 mj 25 cm 30, 300 m Vertical precision 10- 50 cm 30 cm (excl. atmosph .
From page 99...
... Spaceborne laser ranging and altimetry concept.


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