[RSS] LPE-II Launch Vehicle

About the rocket:

The LPE-II launch vehicle is a collaboration between CentaurAerospace and simpleAstronaut, with a two-stage configuration

The first stage uses four FE-7 liquid oxygen methane electric pump cycle engines

The second stage uses an FE-7V liquid oxygen methane electric pump cycle engine

Takeoff mass 20.2t

LEO(300*300km) capacity 1.71t

Load profile:

The flight carried two small 3U satellites called "Alpha"

It is equipped with two solar panels, star sensors, communication antennas and research radar

Activation Group:

AG 1: Automatic launch program

AG 2: Water spray noise reduction

AG 3: Disconnect the device

AG 4: Tower lighting

AG 9: Deployment of satellite solar panels

AG 10: Satellite gyroscope

How to use:

1. Press AG 1 to start the launch program and enter the target orbit data as required on the screen.

2. After completion, press AG 1 again to confirm the launch procedure and wait for orbit.

Launch the satellite by increasing the slider 1 to 100%

Attention:

1. Please try not to use 2 times the speed when the engine is working, so as to avoid posture instability

2. The engine wobbles slightly in flight, which is a normal phenomenon, not a handling or vizzy problem

Have fun!