Propulsion Unha-X (Speculation)
 

Stage

Engines

Thrust s.l.

Isp s.l.

Thrust vac

Isp vac

Propellant

Burn time

Flow rate

Total Imp

kN

N*s/kg

kN

N*s/kg

 

tons

 

t/s

MN*s

1

 Pektusan-A2  (3x2)

2,363.4

2638

2,640.1

2947

UDMH/N2O4

110,85

120

0.8959

326.0

LRE-15 (4)

139.9

2510

153.0

2746

60

0.0557

2

Pektusan-B2 (1x2)

    880.0 2947 UDMH/N2O4 56.74 190 0.2986 167.2
3

LRE-X (4)

    125.0 2501  UDMH/N2O4 11.00 220 0.0500 27.5



"Pektusan-A1"