Spacebus is a fully-reusable manned carrier rocket. It could deliver 12 tourists with more than 15 days of supplies at each launch.

For crew safety, it could escape each second after launch by itself.

This is a highly cost-efficient and safe choice of a fully Reusable manned carrier rocket with 1441.128 tons of takeoff weight. Its LEO Low earth orbit performance of a 335X375km 45 degrees from equator LEO orbit is about 17 tons.

It has 70 percentage of Space Shuttle performance, while its cost less than 25 percentage of Space Shuttle. Why is it much cheaper than shuttle, because unlike the expensive fuel tank of Shuttle is not recoverable, Every solid part of this rocket, including its First Core Stage, its Second stage, its liquid boosters, its Fairings, is all reusable.
Its fuel is also much cheaper and safer than space shuttle because all of its stages use LOX-Kerosene Propellant, which is much cheaper than LOX-LHX and solid Propellant of space shuttle. Its Pressurization gas is also cheaper than the helium of space shuttle, it uses Nitrogen as the pressurize gas of its main fuel tank. It uses Oxygen itself to pressurize its LOX tank using higher temperature than the spoiling point of the LOX.

Interestingly, its launch and reentry is automatically controlled by vizzy program.

It should be used on the Real Solar System planet mod and launched on the real earth mod.

For high orbit deep-space version, refer to:
https://www.simplerockets.com/c/iwA2E8/Shipshuttle-GTO-Version-with-Highshuttle-Reusable-GTO-Upper-Stage

Or link:
Deep-Space Version LEO Launcher Shipshuttle-Base

Launch Vizzy game simulator control:

Just take its throttle to 100 percent 10 seconds before launch, the vizzy program would automatically launch the Spacecraft to a 375km X 335km orbit.

Emergencial Launch Termination control:

Activate Group 2 to terminate the launch each second after launch.

Spacebus fully Recoverable shuttle Reentry game simulator control:

Activate group 2 before Reentry at 150km altitude, and notice the Yaw axis of the craft should be vertical to the ground.
At 125km altitude, automatically bring back solar panels.
At 120km altitude to 100km altitude, Automatically Pitch from 0 degrees to 53 degrees using Reentry RCS.
After several jumps on the atmosphere, keep Pitch Angle 53 degrees.
At 3600mps, shut down RCS and Lock heading on 53 - (45/2700) X (3500 - Velocity Surface) degrees higher Pitch on Vector velocity Surface.
Set the degree of After wings at 90 X (1- (3500 - Velocity Surface)/2100) degrees
At Mach 3 at final, set Pitch = -12. Manually control the heading of final approach.
At Altitude below 200m Altitude above ground, automatically release Landing Gear. Half-manually Final Approach.

Second Stage Reentry game simulator control:

Activate group 2 before Reentry at 150km altitude, and notice the Yaw axis of the craft should be vertical to the ground.
At 125km altitude, automatically bring back solar panels.
At 120km altitude to 100km altitude, Automatically Pitch from 0 degrees to 63 degrees using Reentry RCS.
After several jumps on the atmksphere, keep Pitch Angle 63 degrees.
At Mach 3 at final, Shut down Reentry RCS and Lock heading on 10 degrees higher Pitch on Vector velocity Surface. APU (Auxirilly Power Unit) is powered on.
At 12000m altitude above ground, EXTEND PRIMARY WINGS. Set Pitch = -30 + 0.00375 X (12000- AltitudeAgl)
At Altitude below 8000m, set Pitch = -12. Manually control the heading of final approach.
At Altitude below 200m Altitude above ground, automatically release Landing Gear. Half-manually Final Approach.

Basic game simulator Flight program:

-10s Vizzy program of launch activated, the APU (Auxirilly Power Unit) is powered on.
0s 2 Primary engines of the first stage and the Liquid Reusable Booster (LRB) Ignition and takeoff. Set Roll Angle = 0, Pitch Angle = 90, Heading = 90. Keep setting Throttle 100 percent.
+15s at 235m altitude above ground, Begin programmable turn. Set Roll angle = 0, Pitch Angle = 90 - 0.3 X (AltitudeAgl)^0.5, Heading = 90.
+47s at 3000m altitude above ground, Continue programmable turn. Set Roll Angle = 0, Pitch Angle = 75 - 0.3 X (Altitude - 3000)^0.5, Heading = 90.
+88s at 13000m altitude above ground, Stop programmable turn. set Roll Angle = 0, Pitch Angle = 43, Heading = 90.
+115s at 22687m altitude and 1170mps ground speed, cut off booster throttle, start the preparation of the sepration of boosters. Lock heading on Vector velocity Surface. Keep the throttle of Primary Core 1 Stage Engines at 100 percent.
+118s Liquid Roeusable Booster 3 , 5 sepration.
+119s Liquid Reusable Booster 4, 6 sepration.
+120s Liquid Reusable Booster 1,2 sepration. Set Roll Angle = 0, Set Pitch Angle 43 - 0.12 X (Altitude - 174000)^0.5, Set Heading to the Heading of Vector Veolecity Orbit. Keep the throttle of Primary Core 1 Stage Engines at 100 percent. Keep Roll Angle 0.
+185s at 3685mps Velocity Surface, 68841m altitude, First Stage Sepration. Second Stage Main Engine Ignition, Second Stage Lock heading on Vector velocity Orbit. Keep throttle 100 percent.
+224s at 3781mps Velocity Surface, 109km altitude, Fairings Sepration.
+386s at 5580mps Velocity Orbit, 173.5km altitude, Second Stage Lock heading on 10 degrees higher Pitch on Vector velocity Surface. Keep Roll Angle 0. Because its time to approach is less than 30 seconds. If its time apoapsis is more than 39 seconds, Lock heading on Vector velocity Orbit. If its time approach is less than 30 seconds and its Orbit Speed is less than 6500mps, Second Stage Lock heading on 10 degrees higher Pitch on Vector velocity Orbit.
+489s at 6500mps Velocity Orbit, 169.3km altitude, Second Stage Lock heading on 10 degrees higher Pitch on Vector velocity Surface.
+511s at 7839mps Velocity Orbit, 186.6km Altitude Second Stage Main Engine Cut off, throttle 0 percent, its apoapsis would be 375kms above ground.
+2436s at 7620mps Velocity Orbit, 375km Altitude, its time apoapsis is 25 seconds, Second Stage Main Engine Second Ignition. Second Stage Lock heading on 10 degrees higher Pitch on Vector velocity Surface.
+2440s at 7675mps Velocity Orbit, 375km Altitude, its Second Stage Main Engine Cut off, its periapis would be 335kms Altitude. Automatic Launch Program Shut down. Solar Panels Powered On.

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