ORBITAL ROCKET

Orbital rocket features solid motor first and second stages, and bipropellant third stage. High manufacturability supports high production rates and economies of scale. Minimal infrastructure requirements allow truly flexible launch operations.

SECOND STAGE

EXPENDED FIRST AND SECOND STAGES

RECOVERED UNDER PARACHUTE

ROCKET VARIANTS

  THIRD STAGE

ENABLES HIGH ACCURACY FOR

CUSTOMIZED ORBITAL INSERTION

FIRST STAGE

HIGH ALTITUDE OPERATION REDUCES AMBIENT

PRESSURE VARIANCE IN FLIGHT ENVELOPE

ENABLES GREATER EFFICIENCY FOR FIXED NOZZLE GEOMETRY

PAYLOAD

STANDARDIZED PAYLOAD INTEGRATION VARIANTS

TAILORED TO CUSTOMER REQUIREMENTS

10.05 m
0.838 m
25 kg to 550 km SSO

ORBITAL ROCKET SPECIFICATIONS

HEIGHT
DIAMETER
10.05 meters
0.838 meters
PAYLOAD

PAYLOAD CAPACITIES 

1U = x18
2U = x9
3U = x8
6U = x4
12U = x2
Design Point for Commercial Offering:
25 kg to 550 km SSO
Maximum SSO Payload:
33 kg to 550 km SSO
Maximum Circular Payload:
57 kg to 300 km circular
 

SUBORBITAL ROCKET

Suborbital rocket uses a high performance solid motor to support high manufacturability and streamlined operations.  Motor size can be customized to satisfy mission requirements for apogee and duration in micro gravity.

SUB-ORBITAL ROCKET SPECIFICATIONS

HEIGHT
DIAMETER
PAYLOAD
3 meters
0.31 meters
100 kg to 400 km altitude
3 m
0.31 m