Design a two stage to orbit launch vehicle
The first stage is called the Ferry and the second the Orbiter.
See also: WingedLaunchVehicleDesign, DrawVertices
%-------------------------------------------------------------------------- % Copyright (c) 2019 Princeton Satellite Systems, Inc. % All rights reserved %-------------------------------------------------------------------------- % Since version 2019.1 %-------------------------------------------------------------------------- dO = WingedLaunchVehicleDesign( 'name', 'Orbiter',... 'wing position', 'bottom',... 'hydrogen', 1.5732e+03,... 'oxygen', 9.2502e+03,... 'height', 2.2,... 'width', 2.2,... 'payload length', 0.8,... 'engine length', 2.22,... 'engine diameter', 1.44,... 'fuselage roof height', 0.5,... 'tail height', 2); dO.v(:,3) = dO.v(:,3) - 2.1; dF = WingedLaunchVehicleDesign( 'name', 'Ferry',... 'wing position', 'top',... 'hydrogen', 1.5732e+03,... 'height', 1.5,... 'width', 2.2,... 'payload length', 6,... 'inlet height', 0.5,... 'inlet angle', 60,... 'tail separation', 3,... 'tail angle', 20,... 'tail height', 2); f = dF.f; fO = dO.f + size(dF.v,1); v = [dF.v;dO.v]; f = [f;fO]; v = dF.v; f = dF.f; DrawVertices( v, f, 'SRT', true ); %--------------------------------------