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Auto Credit Based on IntegratedSpaceSystems's HL-2C Idaho with Multi Sat Payload

The North Carolina is a 3 stage launch vehicle that can carry 15 tons of payload to Low Droo Orbit using an automated launch program. The ML-4A uses the V4 ISS Auto Launch Program, which is currently the most advanced iteration of the program.

Stage 1:
4x Raleigh Sea Level Engine
Stage 2:
1x Baltimore Vacuum Engine
Stage 3:
1x Providence Vacuum Engine

Max Payload Mass: 15,000 kg
Fairing Volume: 53 m^3
Software Package: ISSAL V4

GENERAL INFO

PERFORMANCE

  • Total Delta V: 6.3km/s
  • Total Thrust: 3.8MN
  • Engines: 6
  • Wet Mass: 1.77E+5kg
  • Dry Mass: 26,371kg

STAGES

Stage Engines Delta V Thrust Burn Mass
1 4 2.7km/s 3.2MN 1.8m 2.03E+5kg
3 1 2.5km/s 519kN 3.3m 61,920kg
5 1 1.1km/s 87kN 3.8m 21,294kg

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