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RSC "Energia" - Launchers
Russian

Sea Launch Project

High Spots

Intelsat-19 Launch


SC Intelsat-19 is the communication satellite manufactured by Space Systems/Loral (SS/L) company based on Bus 1300 and its mass is 5 600 kg.

Intelsat-19 mission was prepared at the Home Port from April 9 to May 15, 2012.
LV Zenit-2S No. SL33 and Block DM-SL No. 32L were used to launch the Intelsat-19 SC.

Chronology of activities (Moscow Time)

April 9 - May 15, 2012

Home Port activities:

  • LV Zenit-2S No. SL33 electropneumatic tests;
  • LV Zenit-2S No. SL33 integrated tests under the injection program;
  • Block DM-SL No. 32L electropneumatic tests;
  • Block DM-SL No. 32L integrated tests under the injection program;
  • Filling of Block DM-SL No. 32L TCS with coolant;
  • Filling of Block DM-SL No. 32L with kerosine, NT and UDMH and gases;
  • Integrated rehearsal # 0 without the off-nominal situation simulation during the processing;
  • Integrated rehearsal #1 with the off-nominal situation simulation during the processing;
  • SC processing activities;
  • SC filling;
  • Rocket Segment systems and equipment processing;
  • OSC of processing equipment complex and pre-launch processing system under the control of LP ACC;
  • Loading propellant components and compressed gases into ships. Kerosine preparation operations;
  • ILV assembly and testing;
  • ILV reloading from ACS to LP;
  • ILV dry roll-out (installation on the launch pad and critical launch readiness checklist).

 

May 15 - 28, 2012

Launch Platform and Assembly/Command Ship passage to the launch area. Activities in the sea passage phase:

  • Sea tests of the Launch Platform and the Assembly/Command Ship;
  • Integrated rehearsal No. 2 with the ONS simulation during the processing;
  • Integrated rehearsal No. 3 with comprehensive involvement of all the personnel and practically all standard and borrowed launch support and flight tracking facilities;
  • Daily parameter control of Block DM-SL;
  • Status monitoring and daily maintenance of RS systems during the sea passage.
May 28 - June 1, 2012

Launch site activities:

  • Transfer of the Rocket Segment systems and equipment from the state of readiness for the sea passage to the state of readiness for ILV PLP and launch;
  • Assessment of oceanographic conditions;
  • ILV preparation for roll-out and erection on the launch pad;
  • US processing (within ILV);
  • Operations for LP LMC transfer to readiness for the sensor data acquisition and transmission during the launch operations;
  • Integrated checks of the Upper Stage automated flight control system;
  • OSC of processing equipment complex (PEC) and pre-launch processing systems (PLPS) under the control of LP ACC;
  • Kerosine preparation for ILV filling;
  • Search for the Launch Platform optimal orientation;
  • Bringing the launch platform in the launch position;
  • Bringing the assembly and command ship in the launch position;
  • ILV roll-out and erection on the launch pad;
  • ILV electrical checks;
  • Critical launch readiness checklist;
  • SC and PLU launch rehearsal;
  • Checks of communication channels;
  • Personnel evacuation from LP to ACS;
  • PLP including ILV fueling.
June 1, 2012

At 9 hr 22 min 55 sec, Moscow Time (at 22 hr 22 min 55 sec on May 31, 2012, Pacific Daylight Time) ILV Zenit-3SL No. SL33 with Intelsat-19 spacecraft was launched. All flight operations were performed normally. SC Intelsat-19 was injected into the design target orbit.

June 1 - 2, 2012
  • Bringing the equipment in the initial state after ILV launch;
  • Return of the "red team" onboard the LP and the incoming inspection of the launch platform;
  • Bringing the equipment in the state of readiness to the sea passage.
June 2 - 15, 2012

The launch platform and the assembly/command ship passage from the launch area to the Home Port.

LAUNCH RESULTS

Based on TMI data the Intelsat-19 spacecraft has been injected into orbit with the following parameters: (the first apogee passage)

Perigee altitude,
km
Apogee altitude,
km
Inclination,
deg
870.0
35 653.2
0,0

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