NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Satellite tracking and Earth dynamics research programsFollowing an upgrading program, ranging performance capabilities of a satellite-tracking pulsed laser system were assessed in terms of range accuracy, range noise, data yield, and reliability. With a shorter laser pulse duration (2.5 to 3.0 NSEC) and a new analog pulse processing system, the systematic range errors were reduced to 3 to 5 cm and range noise was reduced to 5 to 16 cm and range noise was reduced to 5 to 15 cm on Starlette and BE-C, and 10 to 18 cm on LAGEOS. Maximum pulse repetition rate was increased to 30 pulses per minute and significant improvement was made in signal to noise ratio by installing a 3 A interference filter and by reducing the range gate window to 200 to 400 nsec. The solution to a problem involving leakage of a fraction of the laser oscillator pulse through the pulse chopper was outlined.
Document ID
19840015593
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pearlman, M. R.
(Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1984
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NAS 1.26:173502
NASA-CR-173502
Report Number: NAS 1.26:173502
Report Number: NASA-CR-173502
Accession Number
84N23661
Funding Number(s)
CONTRACT_GRANT: NGR-09-015-002
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available