FLIGHT OVERVIEW

342 Miles (550 km) 

341 Miles  (549 km) 

40,000 Feet  (107 km) 

40,000 Feet  (30 km) 

60,000 Feet  (18 km) 

PAYLOAD

52 KG PAYLOAD DELIVERED

550 KM SUN-SYNCHRONOUS ORBIT

T + 00:08:35

THIRD STAGE

MONO-PROPELLANT LIQUID MOTOR 

ENABLES HIGH-ACCURACY FOR CUSTOMIZED ORBITAL INSERTION

T + 00:08:34

SECOND STAGE 

MISSION ENTERS SOLID PROPELLANT SECOND STAGE 

FIRST AND SECOND STAGES RECOVERED VIA PARACHUTE

T + 00:01:41

FIRST STAGE

ROCKET PROCEEDS THROUGH SOLID FIRST STAGE

SOLID ROCKET PROPELLANT ENSURES POWER AND STABILITY 

T + 00:00:32

HIGH ALTITUDE HOLD AND LAUNCH

60,000 FEET (18 KM) 

5% EARTH SEA-LEVEL ATMOSPHERE

T + 00:00:00 

50,000 Feet  (15 km) 

40,000 Feet  (12 km) 

REGULUS DESCENDS

FULL PLATFORM RECOVERY

TO INCLUDE FIRST AND SECOND ROCKETS

T + 01:00:00

REGULUS ASCENT

SYSTEM CONTROLLED ASCENT PHASE

DURATION DEPENDENT ON MISSION REQUIREMENTS

T - 00:20:00

40,000 Feet  (12 km) 

500 Feet (152 meters) 

100 Feet  (30 meters) 

FLIGHT CORRECTIONS

AEROSTAT, REGULUS, AND ROCKET SYSTEM DEPLOYED

FROM AIR, LAND, OR SEA WITH ZERO FIXED INFRASTRUCTURE

T - 00:60:00

100 Feet (30 meters) 

Ground Level

PLATFORM LAUNCH

AEROSTAT, REGULUS, AND ROCKET SYSTEM DEPLOYED

FROM AIR, LAND, OR SEA WITH ZERO FIXED INFRASTRUCTURE

T - 00:60:00