Sea Launch User's Guide
Sea Launch User's Guide
Sea Launch User's Guide
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8. SPACECRAFT INTEGRATION AND LAUNCH OPERATIONS<br />
Overview<br />
<strong>Sea</strong> <strong>Launch</strong> optimizes the convenience of West Coast spacecraft<br />
processing with a true equatorial launch site.<br />
There are three distinct phases of operations:<br />
• Phase I takes place in the payload processing facility (PPF). This<br />
phase starts with the delivery of the spacecraft to <strong>Sea</strong> <strong>Launch</strong> at<br />
Home Port and includes final processing of the spacecraft,<br />
standalone tests, ordnance installation, fueling, and encapsulation<br />
with the payload fairing.<br />
• Phase II takes place on the assembly and command ship (ACS).<br />
This includes mating the encapsulated spacecraft to the Zenit-3SL<br />
launch vehicle and integrated testing.<br />
• Phase III takes place on the launch platform (LP). While still in<br />
port, the integrated launch vehicle (ILV) is erected and electrical<br />
checkout and RF end-to-end tests are conducted. The LP then<br />
transports the ILV to the equator. Rehearsals are conducted while<br />
in transit. At the launch site the launch vehicle is rolled out to the<br />
launch pad for erection and fueling. The launch is then performed<br />
by an automated system.<br />
Figure 8-1 depicts the overall spacecraft processing flow. A nominal 60-<br />
day processing schedule is shown in figure 8-2. Standard deviations from<br />
the 60 day schedule may be accommodated on a case-by-case basis.<br />
Communication and power service to the spacecraft during integration<br />
and launch preparation is shown in figure 8-3.<br />
Payload Processing Facility<br />
Assembly and<br />
Command Ship<br />
<strong>Launch</strong> Platform<br />
Fueling Cell<br />
Encapsulation Cell<br />
SC<br />
Mechanical and<br />
electrical checkout*<br />
Installation on adapter*<br />
Installation on strongback<br />
assembly*<br />
Zenit and Block DM-SL<br />
buildup and checkout<br />
Payload unit mating*<br />
ILV erection, PLU electrical<br />
checkout, and RF end-toend<br />
test*<br />
Transit to launch site<br />
Rehearsals<br />
SC battery charging*<br />
Ordnance<br />
installation*<br />
Horizontal rotation<br />
PLF encapsulation<br />
RF checkout*<br />
Propellant<br />
Transfer of payload unit to ACS<br />
loading*<br />
*Tasks that directly involve the SC<br />
Integrated test for<br />
complete launch vehicle*<br />
Transfer of launch<br />
vehicle to LP hangar<br />
Figure 8-1. Spacecraft Processing Flow<br />
Closeout operations*<br />
Transfer to pad and<br />
erection<br />
Countdown operations<br />
<strong>Launch</strong><br />
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