Appendix

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Appendix

A. Technical description

1. The main body

Figure 15 Lower part of main body in the wind tunnel.
Schlieren photograph. Langley Research Center, NASA

2. The propellant tank

Figure 16 Cross section of main body and propellant tank

Figure 16a Cross section detail

3. The plug nozzle

4. The helicopters

5. The wheels (traditional)

5. The wheels (workable)

Figure 17 Characteristic positions of "crossed wheels"

Figure 18 Support principle of the wheel segments

Figure 19 Design principle of a wheel with continuous tire

1. System of units

2. Procedure

        (a) Flight conditions

        (b) Structural weights

        Introduction

        Weight changes during the operation

        The influence of technology

        Individual weights

W₁: Main Body
W₂: Main Power Plant
W₃: Radiation Shield
W₄: Helicopter Drive
 

Figure 20 Weights of the main power plant

Figure 21 Weights of radiation shield

Figure 22 Geometry of the helicopter arrangement

W₅: Rotor Weight
W₆: Landing Gear
W₇: Command Capsule

3. Results

Figure 23 Result of the analysis

Figure 24 Dependence of vehicle size on development of main power plant