| Milestone |
Time |
Mission Requirements Review
|
End of April 2005 |
System Requirements Review
|
Mid-June 2005 |
Preliminary Design Review
followed by purchasing processes, detailed satellite design and production of engineering models of the satellite subsystems
|
November 2005 |
Bench tests of engineering models in SSC's laboratories
|
September 2006 |
Vibration tests of the two structural test models
|
December 2006 |
|
Guidance, navigation and control system simulations started in SSC's satellite laboratory
|
October 2006 |
Critical Design Review
|
January 2007 |
Delivery of flight hardware and experiments
|
June-December 2007
|
AIT (Assembly, Integration and Test) of the vehicles and their subsystems started
|
September 2007-April 2008
|
Advanced system tests of the satellites
|
May-October 2008 |
Environmental tests (vibration, thermal cycling, EMC etc)
|
October 2008-February 2009 |
Flight acceptance review
at which it is decided if the satellites are ready for launch
|
May 2009
|
Spacecraft ready for transportation to launch site
|
November 2009
|
| Launch from Yasny (Russia) |
April 2010, but is delayed due to a delayed contract between Russia and Kazakhstan |
AIT took place in the clean room facilities at SSC's engineering center in Solna. Environmental tests at system level were performed at Packforsk near SSC's premises and at Intespace in Toulouse, France.