The ILS Proton Breeze M Specifications
Performance Reference: 6,150 kg to reference PSM at 1,500m/s delta V to GSO
Typical Mission: Approximately 9 hours utilizing a five-burn Breeze M mission design
Stages: Three-stage Proton rocket with restartable upper stage
Structure Type: Monocoque
Materials: Aluminum and composites
Propellants: Nitrogen Tetroxide (N2O4); Unsymmetrical DiMethyl Hydrazine (UDMH)
ILS manages and monitors every mission from inception to liftoff as well as post-launch. Each client works with a dedicated team to provide critical information for each step of the launch process. The mission integration and launch schedules created for customers detail all activities and timing for a successful launch program.
