Commit
            to Launch: Space Shuttle Weather Launch Commit Criteria
            
The
            launch weather guidelines involving the Space Shuttle and expendable
            rockets are similar in many areas, but distinctions are made for the
            individual characteristics of each. The criteria are broadly
            conservative to assure avoidance of possible adverse conditions. The
            criteria are reviewed for each launch. Weather outlooks, which are
            provided by the Cape Canaveral Range Forecast Facility begin at
            Launch-minus-5-days. The outlooks include weather trends and their
            possible effects on launch day.
            During
            the countdown, formal weather briefings occur approximately as
            follows:
            
              
                | L-21
                  hr 0 min: | 
                Briefing
                  for removal of Rotating Service Structure | 
              
              
                | L-9
                  hr 00 min: | 
                Briefing
                  for external tank fuel loading | 
              
              
                | L-4
                  hr 30 min: | 
                Briefing
                  for Space Shuttle Launch Director | 
              
              
                | L-3
                  hr 55 min: | 
                Briefing
                  for astronauts | 
              
              
                | L-0
                  hr 35 min: | 
                Briefing
                  for launch and RTLS | 
              
              
                | L-0
                  hr 13 min: | 
                Poll
                  all weather constraints | 
              
            
            The
            basic weather parameters on the pad at liftoff must be as follows:
            Temperature
            Prior to external tank propellant loading, tanking will not begin if
            the 24-hour average temperature has been below 41 degrees F. After
            tanking begins, the countdown will not continue if the temperature
            exceeds 99 degrees F for more than 30 consecutive minutes.
            After
            tanking begins, the countdown shall not be continued nor the Shuttle
            launched if the temperature is lower than the prescribed minimum
            value for longer than 30 minutes unless sun, wind, and relative
            humidity conditions permit recovery.
            The
            minimum temperature limit in degrees F. is specified by the table
            below and is a function of the five-minute average of temperature,
            wind, and humidity. The table becomes applicable when the observed
            temperature reaches 48°F. In no case may the Space Shuttle be
            launched if the temperature is 35°F or colder.
            
              
              
                Wind
                  Speed Relative Humidity
                
                  | 
                     Knots  | 
                  
                     0-64%  | 
                  
                     65-74%  | 
                  
                     75-79%  | 
                  
                     80-89%  | 
                  
                     90-100%  | 
                
                
                  | 
                     0-1  | 
                  
                     48  | 
                  
                     47  | 
                  
                     46  | 
                  
                     45  | 
                  
                     44  | 
                
                
                  | 
                     2  | 
                  
                     47  | 
                  
                     46  | 
                  
                     45  | 
                  
                     44  | 
                  
                     43  | 
                
                
                  | 
                     3  | 
                  
                     41  | 
                  
                     41  | 
                  
                     41  | 
                  
                     40  | 
                  
                     39  | 
                
                
                  | 
                     4  | 
                  
                     39  | 
                  
                     39  | 
                  
                     39  | 
                  
                     39  | 
                  
                     38  | 
                
                
                  | 
                     5-7  | 
                  
                     38  | 
                  
                     38  | 
                  
                     38  | 
                  
                     38  | 
                  
                     38  | 
                
                
                  | 
                     8-14  | 
                  
                     37  | 
                  
                     37  | 
                  
                     37  | 
                  
                     37  | 
                  
                     37  | 
                
                
                  | 
                     14  | 
                  
                     36  | 
                  
                     36  | 
                  
                     06  | 
                  
                     36  | 
                  
                     36  | 
                
              
              The
              above table can be used to determine when conditions are again
              acceptable for launch if parameters have been out of limits for 30
              minutes or less. If longer than 30 minutes, a mathematical
              recovery formula of the environmental conditions is used to
              determine if a return to acceptable parameters has been achieved.
              Launch conditions have been reached if the formula reaches a
              positive value.
              
             
            Wind
            Tanking will not begin if the wind is observed or forecast to exceed
            42 knots for the next three-hour period. For launch, when the wind
            direction at the launch pad is between 300 degrees and 060 degrees,
            the highest wind allowable is 34 knots. When the wind direction is
            between 150 degrees and 200 degrees, the highest wind allowable is
            20 knots. The peak allowable wind speed is on a descending scale
            between the directions of 060 degrees and 150 degrees, and an
            ascending scale between 200 degrees and 300 degrees.
            The
            upper atmosphere wind profile must conform to either one of two wind
            loading programs developed by the Johnson Space Center. This profile
            is determined by a series of Jimsphere wind balloon releases from
            Cape Canaveral Air Force Station. A final recommendation is made by
            the JSC Launch Systems Evaluation Advisory Team (LSEAT) to the KSC
            launch director at Launch minus 30 minutes. The Space Shuttle will
            not be launched within 30 minutes of the time a determination has
            been made that the upper wind profile will adversely affect the
            performance of the launch vehicle.
            Precipitation
            None at the launch pad or within the flight path.
            Lightning
            (and electric fields with triggering potential):
            Tanking
            will not begin if lightning is observed within five nautical miles
            of the launch pad or is forecast to occur during the next three
            hours.
            Launch
            will not occur if lightning has been detected within 10 nautical
            miles of the pad or the planned flight path within 15 minutes prior
            to launch, unless the source of lightning has moved more than 10
            nautical miles away from the pad or the flight path. The one-minute
            average of the electric field mill network, used to measure electric
            fields, shall not exceed -1 or +1 kilovolt per meter within five
            nautical miles of the launch pad at any time within 15 minutes prior
            to launch.
            The
            above rule need not apply if the following two conditions are
            observed to exist:
            
1.
            There are no clouds within 10 nautical miles of the launch pad. If
            clouds are present they may not have been previously associated with
            a thunderstorm, or associated with convective clouds having tops
            greater than the -4 degrees F. temperature level (approximately
            23,000 feet) during the last three hours. The clouds must be thin
            optically transparent clouds, or a cloud cover less than or equal to
            25% of the sky with tops below or equal to the 41 degrees F.
            temperature level (approximately 10,000 feet).
            2. It
            can be determined that abnormal readings are the result of smoke,
            fog, or a maritime inversion associated with an onshore or
            alongshore wind present over the electric field mills, causing those
            mills located near the ocean to be elevated with a positive polarity
            between 1 and 1.5 kilovolts per meter.
            
            Clouds
            (types known to contain hazardous electric fields) The Space
            Shuttle may not be launched if the planned flight path is through a
            layer of clouds with a thickness of 4,500 feet or greater where the
            temperature of any part of the layer is between 32 degrees F. and -4
            degrees F. This frequently corresponds to the altitudes between
            approximately 13,000 feet and 23,000 feet.
            The
            Space Shuttle may not be launched if the planned flight path is
            through any cloud type that extends to an altitude where the
            temperature is between 32 degrees and -4 degrees F. if this is
            associated with disturbed weather within five nautical miles of the
            flight path. (Again, this may correspond to the region between
            approximately 13,000 feet and 23,000 feet altitude.)
            The
            Space Shuttle may not be launched through an opaque cloud which has
            become detached from a thunderstorm within three hours before
            launch, or within 5 nautical miles of thunderstorm debris clouds not
            able to be monitored by the field mill network, or producing a radar
            return showing light rain.
            The
            Space Shuttle may not be launched through cumulus type clouds with
            tops extending into a temperature 41 degrees F. or colder (located
            at approximately 10,000 feet), or within 5 nautical miles of clouds
            with tops extending higher than the 14 degree F. temperature level
            (located at approximately 18,000 feet).
            The
            Space Shuttle may not be launched through or within 10 nautical
            miles of cumulus type clouds with tops extending higher than the -4
            degree F. temperature level (approximately 23,000 feet), or of the
            nearest edge of any cumulonimbus or thunderstorm cloud including its
            associated anvil.