----+----1----+----2----+----3----+----4----+----5----+----6----+----7----+----8
TSTLOV
----+----0----+----0----+----0----+----0----+----0----+----0----+----0----+----0
COLUMNS FORMAT DESCRIPTION DEFAULT VALUE & UNITS
1-6 A6 TSTLOV - Requests application of an
acceleration due to thermal radiation
emmitted from the louvers on
spacecrafts other than TOPEX.
18-24 I7 Satellite ID (required). 0
25-44 D20.8 Magnitude of the acceleration in the space- 0 m/s**2
craft body fixed frame. component of normal
vector if 1 is specified in columns 13-14)
45-59 D15.3 X component of normal vector of the
acceleration in the spacecraft body-fixed frame.
60-72 D13.1 Y component of normal vector of the
acceleration in the spacecraft body-fixed frame.
73-80 D15.3 Z component of normal vector of the
acceleration in the spacecraft body-fixed frame.
IF CARD OMITTED: no louver accceleration will be applied.
JAN 1990
8912.0
ARC SET - Option Cards