FLIGHT
WHEEL ABRASION EXPERIMENT STATUS REPORT

Last updated: 12 Aug 1997, 10:45 am PST, Data Controller: Henry W. Stone, Allen R. Sirota & Howard J. Eisen

No. Rec Sequence Cmd Runout Sol Pass Comments
1 50410E 4046
2 X 50410E 4158 4 2
3 X 50410E 4161 4 2
4 50510E 5062
5 50510E 5065
6 50510E 5065
7 X 51210B 12067 12 2 Gain = 1
8 X 51210B 12070 12 2 Gain = 1
9 X 51410C 14048 14 1 Gain = 1
10 X 51410C 14051 14 1 Gain = 1
11 X 51810 18083 18 2 Gain = 1
12 X 51810 18086 18 2 Gain = 1
13 X 52110E 21118 21 2 Gain = 1
14 X 52110E 21121 21 2 Gain = 1
15 X 52310D 23114 23 1 Gain = 1
16 X 52310D 23117 23 1 Gain = 1
17 X 52810C 28040 28 1 Gain = 1
18 X 53910C 39055 39 1 Gain = 1
19 X 55310D 3043 53 1 Gain = 1
20 X 55310D 3046 53 1 Gain = 1

No.	Rec	Sequence	Cmd	Runout	Sol	Pass	Comments
1		50410E	4046
2	X	50410E	4158	4	2
3	X	50410E	4161	4	2
4		50510E	5062
5		50510E	5065
6		50510E	5065
7	X	51210B	12067		12	2	Gain = 1
8	X	51210B	12070		12	2	Gain = 1
9	X	51410C	14048		14	1	Gain = 1
10	X	51410C	14051		14	1	Gain = 1
11	X	51810	18083		18	2	Gain = 1
12	X	51810	18086		18	2	Gain = 1
13	X	52110E	21118		21	2	Gain = 1
14	X	52110E	21121		21	2	Gain = 1
15	X	52310D	23114		23	1	Gain = 1
16	X	52310D	23117		23	1	Gain = 1
17	X	52810C	28040		28	1	Gain = 1
18	X	53910C	39055		39	1	Gain = 1
19	X	55310D	3043		53	1	Gain = 1
20	X	55310D	3046		53	1	Gain = 1

Web Page Authors: Henry W. Stone and Allen.R.Sirota

All information on this site, including text and images describing the Rover is copyright © 1997, Jet Propulsion Laboratory, California Institute of Technology and the National Aeronautics and Space Administration.

FLIGHT WHEEL ABRASION EXPERIMENT STATUS REPORT

FLIGHT
WHEEL ABRASION EXPERIMENT STATUS REPORT