ILS Proton Breeze M Launch Vehicle

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)
Gross Liftoff Mass: 705,000 kg (1,554,000 lb)
Total Length: 58.2 m (191 ft), with standard commercial 4.0 m diameter fairing.

The enhanced performance provided by the commercial Proton launch vehicle enables our customers to design and launch heavier and more capable spacecraft while maintaining cost effective mission life times.

Advantages of the ILS Proton Breeze M Launch Vehicle:

• Restartable upper stage for mission optimization - LEO, MEO, GTO, GSO, SSTO
• Compatible with all major commercial spacecraft platforms for dedicated single and multiple launches
• Experience launching dual-use satellites and satellites with hosted payloads
• Demonstrated capability to build and serve space stations

ILS Proton Breeze M Rocket Stages:

• + Payload Fairing
• + Payload Adaptor
• + Breeze M
• + Proton 3rd Stage
• + Proton 1st & 2nd Stage

For further information on ILS Proton please see our Proton Mission Planners’ Guide (PDF, Zipadi (e-reader) ) and our Proton Brochure (PDF, Zipadi (e-reader) ).