Development of a Mass Estimating Relationship Database for ...

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Table of Contents Abstract........................................................................................................................4 Acronyms & Notation.................................................................................................. 5 I Introduction .............................................................................................................. 6 II Background ............................................................................................................. 6 III Approach................................................................................................................ 7 IV Description of Sources........................................................................................... 9 V Future Work .......................................................................................................... 13 VI Acknowledgements.............................................................................................. 13 References.................................................................................................................. 14 1.0 Wing.................................................................................................................1.0-1 2.0 Tail...................................................................................................................2.0-1 3.0 Body.................................................................................................................3.0-1 4.0 TPS ..................................................................................................................4.0-1 5.0 Landing Gear ...................................................................................................5.0-1 6.0 Main Propulsion...............................................................................................6.0-1 7.0 RCS..................................................................................................................7.0-1 8.0 OMS.................................................................................................................8.0-1 9.0 Primary Power .................................................................................................9.0-1 10.0 Electrical Conversion & Distribution ..........................................................10.0-1 11.0 Hydraulics....................................................................................................11.0-1 12.0 Surface Control & Actuators .......................................................................12.0-1 13.0 Avionics.......................................................................................................13.0-1 14.0 Environmental Control & Life Support Systems.........................................14.0-1 15.0 Personnel Equipment ...................................................................................15.0-1 16.0 Dry Weight Margin......................................................................................16.0-1 17.0 Crew & Gear................................................................................................17.0-1 18.0 Payload Provisions.......................................................................................18.0-1 19.0 Cargo (up and down) ...................................................................................19.0-1 Georgia Institute of Technology TRF-2
20.0 Residual Propellants ....................................................................................20.0-1 21.0 OMS/RCS Reserve Propellants ...................................................................21.0-1 22.0 RCS Entry Propellants.................................................................................22.0-1 23.0 OMS/RCS On-Orbit Propellants .................................................................23.0-1 24.0 Cargo Discharged ........................................................................................24.0-1 25.0 Ascent Reserve Propellants .........................................................................25.0-1 26.0 Inflight Losses & Vents ...............................................................................26.0-1 27.0 Ascent Propellants .......................................................................................27.0-1 28.0 Startup Losses..............................................................................................28.0-1 Technology Reduction Factors ..........................TRF-Error! Bookmark not defined. Georgia Institute of Technology TRF-3
Page 1: Development of a Mass Estimating Re
Page 5 and 6: Acronyms & Notation AMLS AVID EMA E
Page 7 and 8: for air-breathing launch vehicles.
Page 9 and 10: Equations that predict this vehicle
Page 11 and 12: . The second stage is a rocket powe
Page 13 and 14: 11. Hawkins [x] This source is focu
Page 15 and 16: 1.0 Wing 1.0 Wing AR - Aspect ratio
Page 17 and 18: 1.0 Wing Reference: 1 Derived from:
Page 19 and 20: 1.0 Wing Reference: 2 Derived for:
Page 21 and 22: 1.0 Wing Reference: 4a Derived from
Page 27 and 28: 1.0 Wing Rt - Wing taper ratio = ti
Page 29 and 30: 2.0 Tail 2.0 Tail AR vert - Aspect
Page 31 and 32: 2.0 Tail Reference: 2 Derived for:
Page 33 and 34: 2.0 Tail Reference: 4a Derived from
Page 35 and 36: 2.0 Tail Reference: 5 Derived from:
Page 37 and 38: 2.0 Tail Reference: 10 Derived from
Page 39 and 40: 3.0 Body N crew - Number of crew N
Page 41 and 42: 3.0 Body Reference: 1 Derived from:
Page 43 and 44: 3.0 Body K t = 0.0030 - aluminum th
Page 45 and 46: 3.0 Body K ns_cowl =2.21 - Ti3Al Be
Page 47 and 48: 3.0 Body S base - Surface area of b
Page 49 and 50: 3.0 Body M ox _ tan ks 0. 0255 = M
Page 51 and 52: 3.0 Body Reference: 4b Derived from
Page 53 and 54:
3.0 Body Reference: 5 Derived from:
Page 55 and 56:
Page 57 and 58:
3.0 Body K thrust = 1.949e-3 - inli
Page 59 and 60:
Page 61 and 62:
3.0 Body M = 0. 5623 Payload bay do
Page 63 and 64:
4.0 TPS 4.0 TPS A acc - Area of adv
Page 65 and 66:
4.0 TPS Reference: 1 Derived from:
Page 67 and 68:
4.0 TPS Reference: 3 Derived from:
Page 69 and 70:
4.0 TPS Reference: 4b Derived from:
Page 71 and 72:
4.0 TPS M = mono _ tan k _ ins 0. 2
Page 73 and 74:
4.0 TPS A body_tps - Wetted area of
Page 75 and 76:
5.0 Landing Gear Reference: 1 Deriv
Page 77 and 78:
Page 79 and 80:
5.0 Landing Gear Reference: 4b Deri
Page 81 and 82:
Page 83 and 84:
5.0 Landing Gear Used M glow for co
Page 85 and 86:
Page 87 and 88:
5.0 Landing Gear Reference: 10c Der
Page 89 and 90:
6.0 Main Propulsion Reference: 1 De
Page 91 and 92:
6.0 Main Propulsion Reference: 2 De
Page 93 and 94:
6.0 Main Propulsion Reference: 4a D
Page 95 and 96:
6.0 Main Propulsion Reference: 4b D
Page 97 and 98:
6.0 Main Propulsion purge V body =
Page 99 and 100:
7.0 RCS 7.0 RCS L - Length of vehic
Page 101 and 102:
7.0 RCS Reference: 2 Derived for: A
Page 103 and 104:
7.0 RCS Reference: 3 Derived from:
Page 105 and 106:
7.0 RCS Reference: 6 Derived from:
Page 107 and 108:
7.0 RCS Reference: 10a Derived from
Page 109 and 110:
8.0 OMS Reference: 1 Derived from:
Page 111 and 112:
8.0 OMS Reference: 3 Derived from:
Page 113 and 114:
8.0 OMS Reference: 10a Derived from
Page 115 and 116:
9.0 Primary Power Reference: 1 Deri
Page 117 and 118:
9.0 Primary Power Reference: 3 Deri
Page 119 and 120:
9.0 Primary Power Reference: 4b Der
Page 121 and 122:
9.0 Primary Power Reference: 10 Der
Page 123 and 124:
10.0 Electrical Conversion & Distri
Page 125 and 126:
Page 127 and 128:
Page 129 and 130:
Page 131 and 132:
Page 133 and 134:
11.0 Hydraulic Systems Reference: 1
Page 135 and 136:
Page 137 and 138:
Page 139 and 140:
12.0 Surface Control & Actuators 12
Page 141 and 142:
12.0 Surface Control & Actuators Re
Page 143 and 144:
Page 145 and 146:
Page 147 and 148:
Page 149 and 150:
13.0 Avionics 13.0 Avionics A body
Page 151 and 152:
13.0 Avionics Reference: 2 Derived
Page 153 and 154:
13.0 Avionics Reference: 4a Derived
Page 155 and 156:
13.0 Avionics Reference: 6 Derived
Page 157 and 158:
13.0 Avionics Reference: 10a Derive
Page 159 and 160:
14.0 Environmental Control & Life S
Page 161 and 162:
Page 163 and 164:
Page 165 and 166:
Page 167 and 168:
15.0 Personnel Equipment Reference:
Page 169 and 170:
Page 171 and 172:
Page 173 and 174:
16.0 Dry Weight Margin 16.0 Dry Wei
Page 175 and 176:
16.0 Dry Weight Margin Reference: 2
Page 177 and 178:
Page 179 and 180:
Page 181 and 182:
Page 183 and 184:
17.0 Crew & Gear Reference: 1 Deriv
Page 185 and 186:
17.0 Crew & Gear Reference: 4a Deri
Page 187 and 188:
17.0 Crew & Gear Reference: 6 Deriv
Page 189 and 190:
18.0 Payload Provisions 18.0 Payloa
Page 191 and 192:
18.0 Payload Provisions Reference:
Page 193 and 194:
20.0 Residual Propellants 20.0 Resi
Page 195 and 196:
20.0 Residual Propellants Reference
Page 197 and 198:
20.0 Residual Propellants Reference
Page 199 and 200:
21.0 OMS/RCS Reserve Propellants 21
Page 201 and 202:
21.0 OMS/RCS Reserve Propellants Re
Page 203 and 204:
22.0 RCS Entry Propellants 22.0 RCS
Page 205 and 206:
22.0 RCS Entry Propellants Referenc
Page 207 and 208:
23.0 OMS/RCS On-Orbit Propellants R
Page 209 and 210:
23.0 OMS/RCS On-Orbit Propellants R
Page 211 and 212:
25.0 Ascent Reserve Propellants 25.
Page 213 and 214:
25.0 Ascent Reserve Propellants Ref
Page 215 and 216:
26.0 Inflight Losses & Vents 26.0 I
Page 217 and 218:
26.0 Inflight Losses & Vents Refere
Page 219 and 220:
27.0 Ascent Propellants Reference:
Page 221 and 222:
27.0 Ascent Propellants Reference:
Page 223 and 224:
28.0 Startup Losses Reference: 1 De
Page 225 and 226:
28.0 Startup Losses Reference: 3 De
Page 227 and 228:
28.0 Startup Losses Reference: 10 D
Page 229:
Reference: 6 Derived from data prov
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