Propellant….. nitrogen tetroxide + unsymmetrical dimethylhydrazine
Propellant mass, kg ….. 10
Dry mass, kg ….. 4
LRTE characteristics:
Sustainer LTRE (1 unit):
Thrust, N…..  600
Pitch, yaw, roll LTRE (4 units):
Thrust, N….. 10
Vacuum specific impulse of one LTRE, m/s …..  3000
Total operating time, s …..  40
Supply voltage, V…..  27
Drain current of each LTRE, A, not over….. 1
Start-up/cut-off time of each LTRE, ms, not over…..  7