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SLR-Mail No.6

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Date:1996-01-02 19:00:00
Sender:Daniel Nugent, Nasa <[Mailed EDC <slrmail@dgfi.badw-muenchen.de>]>
Subject:[SLR-Mail] No. 6: Resurs-O1-3 and Meteor2-21 Tracking
Author:Daniel Nugent, Nasa
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SLR Electronic Mail 1996-01-02 19:00:00 UTC Message No. 6
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Author: Daniel Nugent, Nasa
Subject: Resurs-O1-3 and Meteor2-21 Tracking


Dear Colleagues,

On 31 August 1993, a Russian made Meteor2-21 satellite was placed into a 930
kilometer, 82.5 degree inclination orbit by a Russian launch vehicle. This
satellite is primarily a meteorological satellite with 3-axes stabilization.
On 4 November 1994, a Russian Resurs-O1-3 satellite was launched into a 640
kilometer, sun-synchronous orbit at a 98 degree inclination. Resurs-O1-3
carries two multi-spectral scanners and is primarily for natural resource
studies. Both of these satellites also carry retroreflectors for Satellite
Laser Ranging tracking. For NASA SLR support purposes, the Meteor2-21 and
Resurs-O1-3 satellites are being referred to as Fizeau and Resurs,
respectively.

Fizeau and Resurs have been outfitted with specially designed
retroreflectors to support an experiment to measure the fizeau effect.
Basically, these experiments will be used to measure the speed of light in
a moving reference frame. To do this, the experimental package contains two
quartz and two hollow retro-reflector corner cubes. These cubes are
oriented so that only one cube should be visible at any time to a ground
based observer. Therefore, the pass up-side versus down-side reflected
receive signal strengths are expected to be appreciably different.

Ultimately, the purpose of this support is to determine satellite return
signal strength. Therefore, it is extremely important not to change the
receive signal level once satellite data is being recorded. The problem may
arise where the return signal strength may be so great as to saturate one`s
detector apparatus. In such a case, a determination must be made to either
1) continue tracking, if the saturation is not so severe as to damage one`s
equipment, or 2) steer off the satellite altogether, so as not to corrupt
the energy data measurements already recorded. Again, the importance here
is to maintain a constant receive attenuation configuration. For the
purpose of the experiment, we are not overly interested in the accuracy of
the range measurement, per se; although it is required to maintain an
accurate orbit.

It has been pointed out that some systems have no means to measure laser
return signal strength on a shot-by-shot basis. In these cases, the
analysis uses the return ratio, number of received pulses versus number of
transmitted pulses, as an indication of relative signal strength. The logic
here being that the greater the return signal strength, the greater the
number of returns being recorded. Though these measurements are affected by
viewing conditions, over a period of time visibility effects can be factored
out.

The SATIDEN for Fizeau is 9305501 and for Resurs is 9407401. The Fizeau
satellite support designator is G5050MS and the Resurs designator is
G1333MS. Acquisition data is available from the CDDIS under filenames
FIZ*.TIV and RE3*.TIV for Fizeau and Resurs, respectively. Stations may
download these files from the CDDIS, to verify correct processing of the
TIV, at their convenience. Acquisition data anomalies should be reported to
this office as soon as possible. Fizeau and Resurs support will be
prioritized between Starlette and Ajisai (..., Starlette, Fizeau, Resurs,
Ajisai, ...).

Stations capable of supporting the Fizeau and Resurs missions are requested
to incorporate these satellites into their tracking schedules, as
appropriate. Please direct all questions, comments, and concerns regarding
these experiments or their support requirements to Dr. Viktor Shargorodsky,
Russian Academy of Science, via Natalia N. Parhomenko at
natali@ricimi.msk.su.

Best regards,
Daniel Nugent
Supervisor, Network Operations
NASA Satellite Laser Ranging Program



[Mailed From: EDC ]

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