Generate Pluto lander model
Generate a CAD model of a Pluto lander. Creates power and mass reports of the model and exports it to OBJ.
See also BuildCADModel, CreateBody, CreateComponent, CreateReport, ExportOBJ, ThrusterCAD, PanelFrame, StarCameraBasicModel, Constant, SaveStructure, ShapedStrut, Q2Mat, U2Q, Unit, LandingLegsCAD
Contents
%-------------------------------------------------------------------------- % Copyright (c) 2014 Princeton Satellite Systems, Inc. % All rights reserved. %-------------------------------------------------------------------------- % Since 2016.1 %-------------------------------------------------------------------------- % Multibody switch multiBody = false; arraysStowed = true;
Constants
rhoCarbonFiber = 1600; rhoAluminum = 2700; rhoGlass = 2400; rhoSteel = 8000; rhoTungsten = 15630; inToM = 0.0254; rhoSolarPanel = 63/(8.3*2.3); % Dawn spacecraft areal mass (kg/m2) lToM3 = 0.001; % Liters to cubic meters
Mission information
massFuel = 80; massTotal = 150+massFuel; aRatio = 1.5; gPluto = 0.62; thrust = aRatio*gPluto*massTotal;
Spacecraft hardware parameters
% Thrusters densityADN = 1.1679e+03; % ADN green fuel massTank = massFuel*[1 1]/2; nTanks = length(massTank); volTank = massTank./densityADN; scale = 27.8*0.0254/168; dT = 11.8*0.0254; massThruster = 10.8/2.205; [vT, fT] = ThrusterCAD( [0;0;-1], dT, scale*99, 20, 15*scale, 44*scale, 5*scale ); rThruster = [0;0;0.2]; % Inertia inertia = [1.1565 -0.0074 0.0561;... -0.0074 1.0380 0.02281;... 0.0561 0.0228 0.7354]; % Fuel tank fTank = 49/656; rTank = (volTank/(4*pi/3)).^(1/3); % Bus zBox = 2.4*max(rTank); xBox = 4.8*max(rTank); yBox = xBox; panelThickness = 0.004; xTank = 0.8*max(rTank)*1.3; rATank = [xTank*[1 -1;1 -1];zBox*[1 1]/2]; % Star camera cameraAperture = 12.5; cameraFocalLength = 25.0; cameraLengthSunShade = 35.0; cameraApertureSunShade = 25.0; massCamera = 0.25; rCamera = 0.4*[xBox -xBox;-yBox yBox;zBox zBox]; uC = [0;0;1]; v1 = Unit([1;-1;-1]); v2 = Unit([-1;1;-1]); b1 = Q2Mat(U2Q(uC,v1)); b2 = Q2Mat(U2Q(uC,v2)); bCamera = {b1 b2}; % Omni antennas powerOmni = 2; xOmni = [xBox xBox; yBox -yBox; 0 0]/2; rOmni = 0.002; c = Constant('speed of light')*1000; % m/s fComm = 2e9; % sband lOmni = 0.5*c/fComm; massOmni = lOmni*pi*rOmni^2*rhoAluminum; bOmni = {[1 0 0;0 0 1;0 -1 0] [1 0 0;0 0 -1;0 1 0]}; % IMU LN-200S radiusIMU = 0.0889/2; hIMU = 0.0851; massIMU = 0.748; dIMU.manufacturer = 'Northrop Grumman'; dIMU.name = 'LN-200S'; powerIMU = 12; % Sun Sensors massSunSensor = 0.035; xSunSensor = 0.06; ySunSensor = 0.03; zSunSensor = 0.012; bSunSensor = [1 -1 2 -2 3 -3]; powerSunSensor = 0.6; % Processing boards - 3U CompactPCI boards nBoards = 5; powerBoard = 12; xChassis = 0.16 + 0.02; yChassis = 0.1 + 0.02; zChassis = 0.02*nBoards + 0.02; massChassis = 1; % Solar arrays massSAD = 0.2; solarPanelThickness = 0.004; strutLength = yBox/3; nPanels = 2; panelLength = 1; panelWidth = 2; massSolarPanel = panelLength*panelWidth*rhoSolarPanel; solarPanelEff = 0.295; zSolarWing = zBox/2; arrayMassFront = 0.5*solarPanelThickness*panelLength*panelWidth*nPanels*rhoGlass; arrayMassBack = 0.5*solarPanelThickness*panelLength*panelWidth*nPanels*rhoCarbonFiber; massStrut = 0.1; yPanel = 0.03; bX = [ 1 0 0;0 0 -1;0 1 0]'; bY = [-1 0 0;0 1 0;0 0 -1]; % Battery power = 0.8*2*1000; powerNight = 5; massBattery = powerNight*24*15/135; % Saft batteries volBattery = powerNight*24*15/250; wBattery = (2*volBattery*lToM3)^(1/3); % One length is half the others
Initialize BuildCADModel and create the Core body
BuildCADModel( 'initialize' ); BuildCADModel( 'set name' , 'PlutoLander' ); BuildCADModel( 'set units', 'mks' ); % Core m = CreateBody('make','name','Core'); BuildCADModel('add body', m ); if( multiBody ) rHinge = [0;0;strutLength]; else rHinge = [0;0;0]; end m = CreateBody('make','name','SolarWing','rHinge',rHinge,'previousBody',1); BuildCADModel('add body', m ); if( ~multiBody ) zPanel = zBox+panelWidth/2; zStrut = zBox; end % This creates the connections between the bodies BuildCADModel( 'compute paths' );
Components
if arraysStowed % Stow the arrays with a portion of a panel showing tStowed = 0.1; m = CreateComponent( 'make', 'box', 'x',xBox, 'y',yBox, 'z',tStowed,... 'faceColor', 'aluminum', 'rA', [0;0;zBox+tStowed/2], 'mass', 2*massSolarPanel+massStrut,... 'name','Solar Arrays Stowed', 'body', 2,... 'inside', 0, 'power', 0 ); BuildCADModel( 'add component', m ); m = CreateComponent( 'make', 'box', 'x',xBox, 'y',yBox, 'z',solarPanelThickness,... 'faceColor', 'solar cell', 'rA', [0;0;zBox+tStowed], 'mass', 0,... 'name','Solar Array Face', 'body', 2,... 'inside', 0, 'power', -250 ); BuildCADModel( 'add component', m ); else % Solar Array 1 m = CreateComponent( 'make', 'box', 'x',panelWidth, 'y',nPanels*panelLength, 'z',solarPanelThickness,... 'faceColor', 'solar cell', 'rA', [0;yPanel+panelLength;zPanel], 'mass', massSolarPanel,... 'name','Solar Array +Y', 'body', 2,... 'inside', 0, 'power', -power/2 ); BuildCADModel( 'add component', m ); m = CreateComponent( 'make', 'box', 'x',panelWidth, 'y',nPanels*panelLength, 'z',solarPanelThickness,... 'faceColor', [0 0 0], 'rA', [0;yPanel+panelLength;zPanel-solarPanelThickness], 'mass', 0,... 'name','Solar Array +Y back', 'body', 2,... 'inside', 0, 'power', 0 ); BuildCADModel( 'add component', m ); % Solar Array 2 m = CreateComponent( 'make', 'box', 'x',panelWidth, 'y',nPanels*panelLength, 'z',solarPanelThickness,... 'faceColor', 'solar cell', 'rA', [0;-yPanel-panelLength;zPanel], 'mass', massSolarPanel,... 'name','Solar Array -Y', 'body', 2,... 'inside', 0, 'power', -power/2 ); BuildCADModel( 'add component', m ); m = CreateComponent( 'make', 'box', 'x',panelWidth, 'y',nPanels*panelLength, 'z',solarPanelThickness,... 'faceColor', [0 0 0], 'rA', [0;-yPanel-panelLength;zPanel-solarPanelThickness], 'mass', 0,... 'name','Solar Array -Y back', 'body', 2,... 'inside', 0, 'power', 0 ); BuildCADModel( 'add component', m ); % Vertical strut m = CreateComponent( 'make', 'cylinder', 'rUpper', 0.01, 'rLower', 0.01, 'h', panelWidth/2, 'n', 24, 'rA',[0;0;zStrut],... 'name', 'Motor', 'body', 1, 'mass', massStrut,'power',0, ... 'faceColor', [0 0 0], 'inside', 1); BuildCADModel( 'add component', m ); end
Bus Frame
[v, f] = PanelFrame( xBox, yBox, panelThickness, panelThickness ); massFrame = 2*(xBox + yBox)*panelThickness^2*rhoCarbonFiber; m = CreateComponent( 'make', 'generic', 'vertex', v, 'face', f,... 'faceColor', 'gold foil','rA', [0;0;zBox-2*panelThickness],... 'mass', massFrame, 'name', 'Top Frame', 'body', 1, 'inside', 0 ); BuildCADModel( 'add component', m ); v = ([1 0 0; 0 1 0; 0 0 -1]*v')'; m = CreateComponent( 'make', 'generic', 'vertex', v, 'face', f,... 'faceColor', 'gold foil','rA', [0;0;2*panelThickness],... 'mass', massFrame, 'name', 'Bottom Frame', 'body', 1, 'inside', 0 ); BuildCADModel( 'add component', m ); z1 = 2*panelThickness; z2 = z1 + zBox-2*panelThickness; c = []; c.x = [ -0.250 0 0 0.250 0.250 0 0 -0.250]*inToM; c.y = [ 0.375 0.375 0.125 0.125 -0.375 -0.375 -0.125 -0.125]*inToM; [v, f] = ShapedStrut( [0;0;z1], [0;0;z2], c ); angle = 0; sX = [1 1 -1 -1]; sY = [1 -1 -1 1]; massStrut = panelThickness^2*zBox*rhoCarbonFiber; for k = 1:4 angle = angle + pi/2; xF = sX(k)*(xBox/2 - panelThickness/2); yF = sY(k)*(yBox/2 - panelThickness/2); b = [cos(angle) sin(angle) 0;-sin(angle) cos(angle) 0;0 0 1]; vR = (b*v')'; m = CreateComponent( 'make', 'generic', 'vertex', vR, 'face', f,... 'faceColor', 'gold foil','rA', [xF;yF;0], ... 'mass', massStrut, 'name', ['z strut' num2str(k)], 'body', 1,... 'inside',0 ); BuildCADModel( 'add component', m ); end
Panels
panelName = {'+X' '-X' '+Y' '-Y' '+Z' '-Z'};
color = {'gold foil' 'gold foil' 'gold foil' 'gold foil' 'gold foil' 'radiator'};
xLoc = (xBox - panelThickness)/2;
yLoc = (yBox - panelThickness)/2;
zLoc = (zBox - panelThickness)/2;
wX = xBox - 2*panelThickness;
wY = yBox - 2*panelThickness;
wZ = zBox - 2*panelThickness;
th = panelThickness;
zH = zBox/2;
rAP = [ xLoc -xLoc 0 0 0 0 ;...
0 0 yLoc -yLoc 0 0;...
zH zH zH zH zBox 0];
dP = [ th th wX wX wX wX ;...
wY wY th th wY wY;...
wZ wZ wZ wZ th th];
for k = 1:6
massPanel = dP(1,k)*dP(2,k)*dP(3,k)*rhoCarbonFiber;
m = CreateComponent( 'make', 'box', 'x', dP(1,k), 'y',dP(2,k), 'z',dP(3,k),...
'faceColor', color{k}, 'rA', rAP(:,k), 'mass', massPanel,...
'name', ['Panel ' panelName{k}], 'body', 1,...
'inside', 0 );
BuildCADModel( 'add component', m );
end
% Landing legs
rL = 35;
[v, f] = LandingLegsCAD('scale',0.012,'xy spacing',rL);
m = CreateComponent( 'make', 'generic', 'v',v,'f',f,...
'faceColor', [1 0.84 0] ,'rA', [0;0;0],...
'name', 'Landing Legs','inside',0);
BuildCADModel( 'add component', m );
% Battery
rB = 0.5*([0;yBox;0] + [-2*panelThickness;-wBattery-2*panelThickness;wBattery/2]);
m = CreateComponent( 'make', 'box','x', wBattery, 'y', wBattery, 'z', wBattery/2,...
'faceColor', [0 1 0] ,'rA', rB,'mass',massBattery,...
'name', 'Battery 1','inside',1);
BuildCADModel( 'add component', m );
% Omni antennas
for k = 1:2
m = CreateComponent( 'make', 'cylinder', 'rUpper', rOmni, 'rLower', rOmni, 'h', lOmni, 'n', 24, 'rA',xOmni(:,k),'b',bOmni{k},...
'name', sprintf('Omni %d',k), 'body', 1, 'mass', massOmni,'power',powerOmni, ...
'faceColor', [0 0 0], 'inside', 1);
BuildCADModel( 'add component', m );
end
% Fuel tanks - wet
for k = 1:nTanks
m = CreateComponent( 'make', 'sphere','radius', rTank(k),'n',20,...
'faceColor', [0 1 0] ,'rA', rATank(:,k),'mass',(1+fTank)*massFuel/nTanks,...
'name', sprintf('HPGP Tank %d',k),'inside',1);
BuildCADModel( 'add component', m );
end
% Star cameras
[v, f] = StarCameraBasicModel( cameraAperture, cameraFocalLength, cameraApertureSunShade, cameraLengthSunShade );
m = CreateComponent( 'make', 'generic', 'v', v, 'f', f, 'b', bCamera{1},...
'rA', rCamera(:,1), 'name', 'Star Camera 1', 'body', 1, 'mass', massCamera );
BuildCADModel( 'add component', m );
m = CreateComponent( 'make', 'generic', 'v', v, 'f', f, 'b', bCamera{2},...
'rA', rCamera(:,2), 'name', 'Star Camera 2', 'body', 1, 'mass', massCamera );
BuildCADModel( 'add component', m );
% IMU
rIMU = [ xBox/2-radiusIMU-4*panelThickness;...
yBox/2-radiusIMU-4*panelThickness;...
panelThickness];
m = CreateComponent( 'make', 'cylinder', 'rUpper', radiusIMU, 'rLower',radiusIMU,'h',hIMU,...
'inside', 1,'deviceInfo',dIMU,'mass',massIMU,...
'rA', rIMU, 'name', 'IMU', 'body', 1, 'faceColor', [0 0 1], 'power', powerIMU );
BuildCADModel( 'add component', m );
% Chassis
m = CreateComponent( 'make', 'box', 'x', xChassis, 'y', yChassis, 'z', zChassis, 'faceColor', [0 0.5 0.5],...
'rA', [-xBox/2 + xChassis/2 + 2*panelThickness; -yBox/2 + yChassis/2 + 2*panelThickness; zBox - zChassis/2 - 2*panelThickness],...
'mass', massChassis, 'name', 'C&DH Box', 'body', 1, 'inside', 1 );
BuildCADModel( 'add component', m );
m = CreateComponent( 'make', 'generic', 'v', vT, 'f', fT, 'faceColor', [0 0.5 0.5],...
'rA', rThruster, 'mass', massThruster, 'name', 'Thruster', 'body', 1, 'inside', 0 );
BuildCADModel( 'add component', m );
% Misc payload
rPayload = [xTank*[1 -1;-1 1];zBox*[1 1]/2];
%BuildCADModel( 'update body mass properties' );
g = BuildCADModel( 'get model' );
mPayload = massTotal-g.mass.mass;
for k = 1:2
m = CreateComponent( 'make', 'box', 'x',2*rTank(1), 'y', 2*rTank(1), 'z',2*rTank(1),...
'faceColor', 'magenta' ,'rA', rPayload(:,k),'mass',mPayload/2,...
'name', sprintf('Payload %d',k),'inside',1);
BuildCADModel( 'add component', m );
end
Add subsystems
if 1 BuildCADModel( 'add subsystem', 'ACS', {'star camera','rwa','imu'} ); BuildCADModel( 'add subsystem', 'Propulsion', {'thruster','tank'} ); BuildCADModel( 'add subsystem', 'Telemetry and Command', {'C&DH', 'omni', 'signal','processor', 'antenna', 'board'} ); BuildCADModel( 'add subsystem', 'Power Lander', {'solar array', 'battery', 'motor'} ); BuildCADModel( 'add subsystem', 'Structure', {'legs', 'panel', 'frame', 'strut'} ); BuildCADModel( 'add subsystem', 'Payload', {'payload'} ); end
Update the mass properties to produce the tables
BuildCADModel( 'update body mass properties' ); g = BuildCADModel( 'get model' ); BuildCADModel( 'show vehicle' ) CreateReport( g, 'tex', FileFullpath('PlutoLanderMass'), 'mass', 1, 1, 1 ) CreateReport( g, 'tex', FileFullpath('PlutoLanderPower'), 'power', 1, 1, 1 ) CreateReport( g, 'txt', [], 'mass', 1, 0, false ); CreateReport( g, 'txt', [], 'power', 1, 0, false );
Component Mass Units
ACS subsystem
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
IMU 0.748 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
ACS Subsystem Total 688.8 kg
Propulsion subsystem
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
C&DH Box 1 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Propulsion Subsystem Total 369.1 kg
Telemetry and Command subsystem
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Battery 1 13.33 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Telemetry and Command Subsystem Total 1379 kg
Power Lander subsystem
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Power Lander Subsystem Total 663.4 kg
Structure subsystem
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Landing Legs 0 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload 1 43.27 kg
Payload 2 43.27 kg
Structure Subsystem Total 896.3 kg
Payload subsystem
Solar Arrays Stowed 13.3 kg
Solar Array Face 0 kg
Top Frame 0.09902 kg
Bottom Frame 0.09902 kg
z strut1 0.01238 kg
z strut2 0.01238 kg
z strut3 0.01238 kg
z strut4 0.01238 kg
Panel +X 2.918 kg
Panel -X 2.918 kg
Panel +Y 2.918 kg
Panel -Y 2.918 kg
Panel +Z 5.886 kg
Panel -Z 5.886 kg
Landing Legs 0 kg
Battery 1 13.33 kg
Omni 1 0.002543 kg
Omni 2 0.002543 kg
HPGP Tank 1 42.99 kg
HPGP Tank 2 42.99 kg
Star Camera 1 0.25 kg
Star Camera 2 0.25 kg
IMU 0.748 kg
C&DH Box 1 kg
Thruster 4.898 kg
Payload Subsystem Total 143.5 kg
Total 4140 kg
Component Power On Power Standby Units
ACS subsystem
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
ACS Subsystem Total -714 0 W
Propulsion subsystem
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Propulsion Subsystem Total -468 0 W
Telemetry and Command subsystem
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Telemetry and Command Subsystem Total -1408 0 W
Power Lander subsystem
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Power Lander Subsystem Total -452 0 W
Structure subsystem
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload 1 0 0 W
Payload 2 0 0 W
Structure Subsystem Total -936 0 W
Payload subsystem
Solar Arrays Stowed 0 0 W
Solar Array Face -250 0 W
Top Frame 0 0 W
Bottom Frame 0 0 W
z strut1 0 0 W
z strut2 0 0 W
z strut3 0 0 W
z strut4 0 0 W
Panel +X 0 0 W
Panel -X 0 0 W
Panel +Y 0 0 W
Panel -Y 0 0 W
Panel +Z 0 0 W
Panel -Z 0 0 W
Landing Legs 0 0 W
Battery 1 0 0 W
Omni 1 2 0 W
Omni 2 2 0 W
HPGP Tank 1 0 0 W
HPGP Tank 2 0 0 W
Star Camera 1 0 0 W
Star Camera 2 0 0 W
IMU 12 0 W
C&DH Box 0 0 W
Thruster 0 0 W
Payload Subsystem Total -234 0 W
Total -4212 0 W
Export to and obj (graphics) file
if arraysStowed SaveStructure(g, FileFullpath('PlutoLander-Stowed')); else ExportOBJ( g, FileFullpath('PlutoLander')); SaveStructure(g, FileFullpath('PlutoLander')); end %-------------------------------------- % PSS internal file version information %--------------------------------------