Spacecraft Thermal Control Handbook, VolumeI: Fundamentals Technologies

Nomenclature

a

contact radius; outer radius in Roca and Mikic mechanical model; heat-flux radius at top of doubler, Gluck and Young (m)

A

area (m 2)

A b

area of contact region near bolt or screw (m 2)

A N

area divided by number of bolts or screws (m 2)

b

component radius; doubler radius, Gluck and Young (m)

C

conductance (W/K)

C b

bolt region conductance (W/K)

CCD

charge-coupled device

CTE

coefficient of thermal expansion (K 1)

d

height of waviness represented as spherical crown; gas gap between parallel plates; distance between bolt centers (m)

d*

normalized distance between bolt centers, d* = d/(2 r O)

D s

bolt-shaft diameter (m)

DLR

Deutsches Zentrum f r Luft-und Raumfahrt e.V. /German Aerospace Center

E

elastic modulus; effective elastic modulus, Roca and Mikic (N/m 2)

E ?

effective elastic modulus (N/m 2),

f

factor from Song representing Integral model of Yovanovich,

F

heat flux (W/m 2)

F O

average heat flux through doubler, Gluck and Young (W/m 2)

F S

heat flux over radius, a, at top of doubler, Gluck and Young (W/m 2)

F*

dimensionless heat flux, Ayres et al., F* = ( F ? ER E/k E) ( E E/H E) ( ? i/ ? o) 3[0.5(1 + P amb/ P atm)] 2

G

dimensionless gap resistance, G = k g

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