Spacecraft Thermal Control Handbook, VolumeI: Fundamentals Technologies

| 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 |