PDS_VERSION_ID                        = PDS3                                  
RECORD_TYPE                           = FIXED_LENGTH                          
RECORD_BYTES                          = 80                                    
FILE_RECORDS                          = 51                                    
DATA_SET_ID                           = "MGN-V-RSS-1-BSR-V1.0"                
PRODUCT_ID                            = "94151151.QPC"                        
FILE_NAME                             = "94151151.QPC"                        
SPACECRAFT_NAME                       = MAGELLAN                              
INSTRUMENT_ID                         = RSS                                   
TARGET_NAME                           = "VENUS"                               
PRODUCT_VERSION_ID                    = 1                                     
PRODUCT_CREATION_TIME                 = 1994-05-25T14:08:23                   
MISSION_PHASE_NAME                    = "MAPPING CYCLE 6"                     
ORBIT_NUMBER                          = {12955,12956,12957,12958}             
START_TIME                            = 1994-05-31T10:00:00                   
STOP_TIME                             = 1994-05-31T20:00:00                   
SPACECRAFT_CLOCK_START_COUNT          = "N/A"                                 
SPACECRAFT_CLOCK_STOP_COUNT           = "N/A"                                 
^DESCRIPTION                          = "QTERNION.TXT"                        
NOTE                                  = "The pre- and post-experiment         
    calculated values of the attitude quaternions, just prior to the          
    first experiment and just after the last experiment were:                 
                                                                              
            Date/Time (SCET)       Q1         Q2         Q3         Q4        
          -------------------  ---------- ---------- ---------- ----------    
          94-151/12:26:25.933   0.6502909 -0.5343113  0.4328263  0.3229431    
          94-151/17:07:43.268   0.6509592 -0.5333617  0.4339242  0.3216908    
                                                                              
    The polynomial execution times (TTF, in SCET) for each orbit are:         
                                                                              
          Orbit 12955:                                                        
          94-151/12:26:25.933  Start Spotlight Pointing                       
          94-151/12:27:48.266  OB 12955 Polynomial Reference Time             
          94-151/12:28:51.266  End Spotlight Pointing                         
               Attitude Knowledge Error= 0.150 degrees                        
                                                                              
          Orbit 12956:                                                        
          94-151/13:59:23.267  Start Spotlight Pointing                       
          94-151/14:00:45.666  OB 12956 Polynomial Reference Time             
          94-151/14:01:48.600  End Spotlight Pointing                         
               Attitude Knowledge Error= 0.137 degrees                        
                                                                              
          Orbit 12957:                                                        
          94-151/15:32:20.601  Start Spotlight Pointing                       
          94-151/15:33:43.066  OB 12957 Polynomial Reference Time             
          94-151/15:34:45.934  End Spotlight Pointing                         
               Attitude Knowledge Error= 0.145 degrees                        
                                                                              
          Orbit 12958:                                                        
          94-151/17:05:17.935  Start Spotlight Pointing                       
          94-151/17:06:40.466  OB 12958 Polynomial Reference Time             
          94-151/17:07:43.268  End Spotlight Pointing                         
               Attitude Knowledge Error= 0.137 degrees "                      
                                                                              
END