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Configuration 1: Configuration 2: Configuration 3: Configuration 4: One Pod No Escape Two Pods No Escape One Pod Bailout System One Pod Propulsion Bailout System Configuration 5: Configuration 6: Configuration 7: Configuration 8: Two Pods Bailout Systems Two Pods Propulsion Bailout Systems Two Pods Propulsion / Bailout Systems Three Pods Bailout Systems Critical Design Review Page 3
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shoulder roll shoulder pitch elbow roll elbow pitch wrist roll wrist pitch wrist yaw tool drive roll 0.68m 0.68m 0.17m Critical Design Review Page 5
Bare Bolt Drive Critical Design Review Page 6 Parallel Jaw Mechanism http://rtsx.ssl.umd.edu Microconical
shoulder roll shoulder pitch elbow roll elbow pitch wrist roll wrist pitch 1.36m 1.36m 0.17m Critical Design Review Page 7
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1 7,8 6 2,3 4,5 Critical Design Review Page 9
12 10 9 14 13 11 Critical Design Review Page 10
19 20 21 Grapple Arm 22 Task Arm 16 15 17 18 Critical Design Review Page 11
26, 27, 28 Not Shown 25 23 24 Critical Design Review Page 12
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Operation: Laser diodes illuminate retro-reflectors mounted on the target CMOS camera detects reflected beams from target DSP translates video information and converts it into relative position and attitude measurements SBC sends information to Guidance, Navigation, and Control (GN&C) system Activ e Sensor Retro-Reflector Clusters Passiv e Target Critical Design Review Page 15
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Gimbaled Omni Ka-Band Video System Video Displays Antenna Switch Diplexer Flight computers FDCC FDCC FDCC Crew Interface - Hand Controllers - Switches - Voice Power Amplifier Low Noise Amplifier Sensor Data Transponder Avionics Critical Design Review Page 17
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Component Mass (kg) Power (W) Maturity CompactPCI Box - 6U Chassis 15 N/A Estimated FDCC Single-Board Computers (3) 1.647 20.4 Measured Solid State Recorder Card (2) 1.84 12 Measured IEEE 1394 Data Bus Card (2) 1.84 10 Measured Video Display Graphics Card (2) 2 10 Measured Open CompactPCI Card Slot (5) 5 30 Estimated Crew Interface Display - 15" (2) 14.6 52 Measured Keyboard and Hand Controllers (2) 5.35 1 Estimated Heads-Up-Display Electronics 2 5 Estimated Crew Interface Switches 6.3 1 Estimated Internal and External Cameras 1.5 9 Measured Camera Gimbals 10 30 Measured Power Distribution Unit (3) 30 15 Estimated Wiring Harness 50 N/A Calculated Total 191 295 Avionics Critical Design Review Page 19
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Top Left Panel (T8) GN 2 (P) (P) GN 2 Top Right Panel (T4) (P )(T) Fill and Drain Valve Flow Control Valve Normally Closed Flow Control Valve Normally Open Filter Thrust Chamber Valve (TCV) Valve Branch A Valve Branch B Heater Pressure Temperature Thruster Isolation Valve (T6) (T7) (T5) Bottom Left Panel (T16) (T14) (T15) 1A 3A (T) (T) (P) N 2 H 4 N 2 H (T) 4 6A 4A 2 (P) (T) 1B 5 3B 4B 6B Bottom Right Panel (T2) (T3) (T1) (T12) (T10) (T11) (T13) (T9) Valve Heaters Line Heaters Critical Design Review Page 21 Catalyst Bed Heaters
Top Left Panel (T8) (T6) Fill and Drain Valve (P) (P) Flow Control Valve (T7) (T) (T) Normally Closed N 2 N Flow Control Valve 2 Normally Open (T5) Filter Thrust Chamber Valve (TCV) Bottom Valve Branch A Left Panel Valve Branch B 1A 4A 1B 4B Heater (T16) (P Pressure )(T) R1 R2 R3 R4 (T14) 2 Temperature Thruster Isolation Valve Pressure Regulator Relief Valve (T15) (T13) 5 3A 6A 3B 6B Top Right Panel (T4) Bottom Right Panel (T2) (T3) (T1) (T12) (T10) (T11) (T9) Critical Design Review Page 22
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Critical Design Review May 3, 2003 Critical Design Review Page 24