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Development of a Mass Estimating Relationship Database for ...

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1.0 Wing<br />

b body – Maximum width <strong>of</strong> the body<br />

b str – Wing structural span along the half chord line<br />

M land – Landed mass <strong>of</strong> vehicle<br />

N z – Ultimate load factor = 1.5*2.5 (factor <strong>of</strong> safety * limit load)<br />

S body – Plan<strong>for</strong>m area <strong>of</strong> the body<br />

S exp – Exposed wing plan<strong>for</strong>m area<br />

t root – Wing thickness at root<br />

Georgia Institute <strong>of</strong> Technology 1-4

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