ISTP  MEASUREMENTS OF
ION UPFLOW MECHANISMS

 
DATE
INTERVAL (UT)
MLT = UT - 02
SPACECRAFT
CONJUNCTION
Aug 06, 1998
1945 - 2230
FAST
Aug 07, 1998
0815 - 1130
Akebono
Aug 08, 1998
0800 - 1015
Akebono
Aug 09, 1998
0800 - 1015
Akebono
Aug 10, 1998
0730 - 0915
Akebono
Sep 05, 1998
1630 - 1845
FAST
Sep 10, 1998
1615 - 1845
FAST
Nov 12, 1998
1015 - 1245
FAST
Dec 05, 1998
2030 - 2300
Akebono
Jan 08, 1999
1415 - 1930
FAST & Akebono
Aug 10, 2001
1740-2300
FAST
Aug 11, 2001
0400-1000
POLAR
Aug 24, 2001
1540-2100
FAST
Aug 27, 2001
1540-2050
FAST
Sep 02, 2001
1420-1650
POLAR
Sep 29, 2001
0030-0600
FAST & POLAR
Oct 11-12, 2001
2330-0450
POLAR
Oct 21-22, 2001
1530-0400
FAST & POLAR
Nov 10-11, 2001
2130-0500
FAST
Nov 26-27, 2001
1730-0005
FAST & POLAR
Dec 09-10, 2001
1830-0005
POLAR

 

Antenna mode:

The antenna cycled through two 10-min composite scans (one east, one west) and a
10-minute dwell parallel to B.  The composite scans were performed with
a variable scan rate that gives constant ground tracking.  The complete
cycle time was just under 31m30s.
 
 

Transmitter mode:

Dual longpulses, merged.  Although the data are fully sampled
every 21 km, the resolution of the pulselength is 48 km.
 
 

Range integration:

The data were range integrated for
 21 km up to 200 km altitutude,
 42 km from 200 to 400 km altitude, and
 63 km above 400 km altitude
(although the best resolution of the data is 48 km).
 
 

Time integration:

The data were integrated on-line for 10 sec, and were integrated for
processing as follows.
The dwell data were integrated for 3m20s (200s), giving 4 records for
each 10-min dwell up B.  The scan data were integrated for 60s, giving
10 records for each scan.