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Prelaunch testing of the laser geodynamic satellite (LAGEOS)The LAGEOS was extensively tested optically prior to launch. The measurement techniques used are described and resulting data is presented. Principal emphasis was placed on pulse spreading characteristics, range correction for center of mass tracking, and pulse distortion due to coherent effects. A mode-locked freqeuncy doubled Nd:YAG laser with a pulse width of about 60 ps was used as the ranging transmitter and a crossfield photo-multiplier was used in the receiver. High speed sampling electronics were employed to increase receiver bandwidth. LAGEOS reflected pulses typically had a width of 250 ps with a variability in the range correction of less than 2 mm rms. Pulse distortion due to coherent effects was inferred from average waveforms and appears to introduce less than + or - 50 ps jitter in the location of the pulse peak. Analytic results on this effect based on computer simulations are also presented. Theoretical and experimental data on the lidar cross section were developed in order to predict the strength of lidar echoes from the satellite. Cross section was measured using a large aperture laser collimating system to illuminate the LAGEOS. Reflected radiation far-field patterns were measured using the collimator in an autocollimating mode. Data were collected with an optical data digitzer and displayed as a three-dimensional plot of intensity versus the two far-field coordinates. Measurements were made at several wavelengths, for several types of polarizations, and as a function of satellite orientation.
Document ID
19780002257
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Fitzmaurice, M. W.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Minott, P. O.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Abshire, J. B.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Rowe, H. E.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1977
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
NASA-TP-1062
G-7702-F16
Report Number: NASA-TP-1062
Report Number: G-7702-F16
Accession Number
78N10200
Funding Number(s)
PROJECT: RTOP 506-20-33
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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