NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
ISEE-3/ICE navigation analysisEfforts to assure communications continuity and navigational accuracy for the ISEE-3 (now called the International Cometary Explorer - ICE) spacecraft as it heads toward a passage through the Giacobini-Zimmer (G-Z) comet tail are reviewed. Sufficient energy was gained with a series of lunar swingbys to take the rendezvous attempt possible. Communications will be by an S-band link though the upgraded Deep Space Network. The G-Z encounter is scheduled for September 1983. A 512 bps data rate will be supported by 64-3 m dishes at various global sites. The tracking will continue for 6 mos as the spacecraft moves into an orbit that parallels that of Halley's Comet. Ground-based recovery of the G-Z location in the spring of 1984 provided data for calculating the ephemerides required for configuring a major course correction for ICE 100 days before rendezvous.
Document ID
19840061421
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Efron, L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ellis, J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Yeomans, D. K.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Chodas, P. W.
(California Institute of Technology, Jet Propulsion Laboratory, Navigation Systems Section, Pasadena CA, United States)
Premkumar, R. I.
(Federal Electric Corp. Pasadena, CA, United States)
Date Acquired
August 12, 2013
Publication Date
August 1, 1984
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
AIAA PAPER 84-1981
Report Number: AIAA PAPER 84-1981
Accession Number
84A44208
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available