|Mission Timeline: Launch - archived
View Detailed Launch Information - archived
Launch phases begin when the spacecraft transfers to internal power on the launch pad and ends when the spacecraft is declared stable, healthy, ready to accept commands and the launch telemetry has been played back.
Rover A launched using a Delta II 7925 launch vehicle from Space Launch Complex 17A (SLC-17A) at the Cape Canaveral Air Force Station in Florida. Rover B launched using a Delta II 7925H launch vehicle from SLC-17B at the Cape. For details, see the launch vehicle in the spacecraft section.
The launch periods for each rover were as follows:
||June 5, 2003
||June 24, 2003
||January 4, 2004
||June 25, 2003
||July 15, 2003
||January 25, 2004
To allow changeover of ground equipment at the launch pads, the two missions must be launched at least 10 days apart. There were two daily launch opportunities throughout both launch periods, providing a high probability of liftoff within the back-to-back MER launch periods. A constant arrival date is used for both rovers.
The major activities in this mission phase included:
- the liftoff and boost phase of the launch
- insertion into a circular parking orbit
- a coast period followed by additional launch vehicle burns necessary to inject the spacecraft onto a trajectory to Mars
- separation of the spacecraft from the launch vehicle
- initial acquisition by the Deep Space Network
- verification of the initial spacecraft health and operating conditions
- the verified execution of a minimal set of post-launch commands