GALACTIC ENERGY

FAIRING

Von Karman Shaped ; Composite Material

LOAD MASS

8t To 200km LEO

17.5t 200km LEO ( two-stage rocket+Eros upper stage))

LOAD SPACE

4.2m Diameter

8m Height

Advanced liquid upper stage

one rocket multi-satellites Space ferry Active derailment

Second stage

Single CQ-50 liquid engine

60t Thrust

330s Vacuum specific impulse

First Stages

Seven CQ-50 liquid engine

7 Engine

135s Work duration

350t Thrust at sea level

265s Vacuum specific impulse

LOX / Kerosene Propellant

Vertical recycling Reusable

Pallas-1 is a two-stage liquid and advanced upper stage reusable carrier rocket independently designed by Galactic Energy. The first and second stages with the CQ-50 liquid oxygen/kerosene engines, the rocket diameter of 3.8m, a total length of 42m, a lift-off mass of 283t, a LEO orbit carrying capacity of 8t.
FLIGHT ENVIRONMENT

Maximum longitudinal overload <7g
Wenchang Taiyuan

INJECTION ACCURACY

Deviation of half length axis ≤5km
Orbital tilt Angle deviation ≤0.05°
Eccentricity deviation ≤0.002

SATELLITE SEPARATION ATTITUDE ANGLE AND ANGULAR RATE DEVIATION

Attitude angle deviation ≤1 °
Attitude angle rate deivation ≤0.3°/s
INTERFACE

Military standard GJB4228 (GJB/Z200) type 300 ~ 2100 type wrap belt spring type satelliteand launch vehicel connection separation unit;
The international general CubeSat release mechanism,can load the common volume of 1U, 2U, 3U, 6U, 12U CubeSat.
Lightweight wrap belt, interface sizes range from 8 to 38 inch in diameter
Explosive bolts, 3-point or 4-point interface
Other interface types.
Multi-satellite
Ample space
Multiple interfaces

PALLAS-1