Theseus II Mark VI SHLLV

Im Bacc bruh 🗿

anyways sorry for the low quality thumbnail,the pic i shot was too far from the rocket lol

alright,to the point

Theseus II Block VI

Is a fictional proposal of a Super Heavy Lift Launch Vehicle,capable to bring 100 Metric ton Payload into the Moon's Orbit with a calculated path.It had a total of 8 Engines at the First Stage(Including 4 SRBs),and A single Hi-Efficiency Vacuum Engine at Its 2nd stage,To accomodate the mass of over 730 Metric Tons.This Project was discontinued due to the Advancement of cheaper reusable rockets.

According to The Proposal,it had 4 Massive H7-N Hyperion Mark II Engines at its Core Stage,and Also 4 SRBs.Total Thrust of the first stage is 24 Mega Newtons (rounded up).The Second Stage,however,uses a single modified H7-N Engines that focuses on vacuum efficiency,with an Isp of 400 seconds,its performance was more than enough to put a heavy payload even on the geostationary orbit.To Assist the vacuum performance,the designers have 4 Maneuvering Thrusters and a bunch of Reaction Control Nozzles.All liquid engines on the craft are using LH/LOX(Hydrolox) as the propellant,combining Liquid Hydrogen as the main fuel and Liquid Oxygen as the Oxidizer.this enhance the vacuum capabillty of this rocket.

Specifications:

I.Mass: 730 tons (W/Propellants)

II.Engines:

•4 x H7-N Core Engine(4 x 3,8-4 MN)

•4 x SRB (4 x 2MN)

•1 x H7-N Vacuum Engine (6 MN)

III.Price: 170 Million Dollars

IV.Dimensions:

•Height:85 m

•Width:12 m

•Depth:15 m

V.Total Thrust:36 MN

VI Total Delta V:98.1 Km/s

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This Craft was tested on RSS,ESS,And Juno system.

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Alright folks,this is what i have for this month,3 weeks from now i would have a good amount of free time,see you next time!