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Auto Credit Based on mvm6's Juno II Ultra Heavy Launch VehicleB

Dear members of the group, Junuo Hang Meng New Group Workshop Announcement:

Hello everyone! We are pleased to share with you our latest achievements and future plans.

First, let's review the Juno II Ultra Heavy Launch Vehicle. The following is basic information about the normal payload of the Juno II superheavy launch vehicle:

  • Name of rocket: Juno II Ultra Heavy Launch Vehicle
  • Price: $2.1B
  • Total mass: 28.4 kilotons (kt), include payload weight
  • Dimensions:
  • Width: 25.4 m
  • Height: 165 m
  • Depth: specific value to be determined
  • Performance parameters:
  • Phase I: 68 seconds burning time, thrust-to-weight ratio 3.32: 1, speed increment 2.36 m/s
  • Phase 2: 0 second burning time, thrust-weight ratio 0. 00: 1, speed increment 0. 00 M/s (may indicate that this stage is not working or is a secondary stage)
  • Phase III: 31 seconds burning time, thrust-to-weight ratio 4.37: 1, speed increment 1.35m/s
  • Stage 4: 8 seconds burning time, 4.37: 1 thrust-to-weight ratio, 1.35m/s speed increment
  • Phase V: 8 seconds burning time, thrust-to-weight ratio 5.12: 1, speed increment 399 m/s
  • Phase 6: 8 seconds burning time, thrust-to-weight ratio 5.12: 1, speed increment 399 m/s

Then we launched a modified version of the Juno II B-Super Heavy Launch Vehicle. The rocket is designed for Earth orbit launch missions and has the following main features and capabilities:

  • Payload capacity: capable of carrying up to 53.4 kilotons of payload.
  • Thrust: A takeoff thrust of 3,117 Mega Newtons.
  • Dimensions: The width, height and depth of the rocket are 25.4 meters.
  • Component composition: consisting of 43 main components.
  • Propulsion systems: liquid oxygen and methane as propellants.
  • Performance indicators: A total speed increment of 2.065 km/s for the three-stage propulsion system for Earth orbit launch missions.

Due to its superior thrust and massive payload capacity, the Juno II B Super Heavy Launch Vehicle is particularly suitable for Earth orbit launch missions requiring high payload capacity. Although how far into Earth orbit the payload can be launched is not detailed, its design and performance indicators show that it can handle the difficult deployment requirements of Earth orbit.

We are also pleased to announce that the Juneau 2 superheavy carrier rocket has been manufactured and the date of its maiden flight is still pending. The maximum payload is 53.4 tons and the minimum payload is 28.3 tons. In addition, the Juneau III B-1001 superheavy rocket is also under construction, with an estimated payload of as little as 100 tons and as much as 112 tons. More details will be made available gradually.

Stay tuned for the latest and look forward to the stunning debut of Juno III's B-1001 superheavy rocket. Thank you for your support, let us look forward to the future of Juno Airlines!

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Zhu Nuo Hang Meng Xintuan Studio

GENERAL INFO

PERFORMANCE

  • Total Delta V: 4.2km/s
  • Total Thrust: 13,919,430.1MN
  • Engines: 17
  • Wet Mass: 2.82E+7kg
  • Dry Mass: 2.27E+7kg

STAGES

Stage Engines Delta V Thrust Burn Mass
1 5 2.4km/s 924.8MN 68s 2.82E+7kg
2 0 0m/s 0N 0s 2.58E+7kg
3 3 1.4km/s 1,043.7MN 31s 2.41E+7kg
5 5 404m/s 1,148.1MN 8s 2.26E+7kg

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