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Critical Design Review – Page 3
University of Maryland
ENAE 484 Spring 2003
Configuration 1: Configuration 5:•One Pod•No Escape
•Two Pods•Bailout Systems
Configuration 2: Configuration 6:• Two Pods• No Escape
• Two Pods• Propulsion
Bailout Systems
Configuration 3: Configuration 7:•One Pod•Bailout System
• Two Pods• Propulsion /
Bailout Systems
Configuration 4: Configuration 8:• One Pod• Propulsion
Bailout System
• Three Pods• Bailout Systems
Critical Design Review – Page 5
University of Maryland
ENAE 484 Spring 2003
0.17m
0.68m 0.68m
shoulder rollshoulder pitchelbow roll
wrist pitchwrist yawtool drive roll
elbow pitchwrist roll
Critical Design Review – Page 6
University of Maryland
ENAE 484 Spring 2003
Bare Bolt Drive
Parallel Jaw Mechanism
Microconicalhttp://rtsx.ssl.umd.edu
Critical Design Review – Page 7
University of Maryland
ENAE 484 Spring 2003
0.17m
1.36m 1.36m
shoulder rollshoulder pitchelbow roll
wrist pitch
elbow pitchwrist roll
Critical Design Review – Page 11
University of Maryland
ENAE 484 Spring 2003
Grapple Arm
221920 21
Task Arm
1615 17
18
Critical Design Review – Page 12
University of Maryland
ENAE 484 Spring 2003
23 24
25
26, 27, 28
Not Shown
Critical Design Review – Page 15
University of Maryland
ENAE 484 Spring 2003
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
Retro-Reflector Clusters
Active Sensor
Passive Target
Critical Design Review – Page 17
University of Maryland
ENAE 484 Spring 2003
Sensor Data
Omni
Video System
Crew Interface - Hand Controllers - Switches - Voice
GimbaledKa-Band
Flight computers
PowerAmplifierFDC
C
FDCC
FDCC
Video Displays AntennaSwitch
Diplexer
Transponder
Low NoiseAmplifier
Avionics
Critical Design Review – Page 19
University of Maryland
ENAE 484 Spring 2003
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 21
University of Maryland
ENAE 484 Spring 2003
Catalyst Bed Heaters
Valve Heaters Line Heaters
(T16)
(T14)
(T15)
(T13)
(T8)
(T6)
(T7)
(T5)
(T4)
(T2)
(T3)
(T1)
(T12)
(T10)
(T11)
(T9)
Bottom Left Panel
Bottom Right Panel
TopLeft Panel
TopRight Panel
Fill and Drain ValveFlow Control Valve Normally ClosedFlow Control Valve Normally OpenFilterThrust Chamber Valve (TCV)Valve Branch AValve Branch BHeaterPressureTemperatureThrusterIsolation Valve
(P)(T)
GN2GN2
(P)
(T) (T)
(P)
1A 4A
3A6A
6B
4B1B
3B
25
N2H4N2H4
(P)(T)
(T)
(P)
Critical Design Review – Page 22
University of Maryland
ENAE 484 Spring 2003
(T16)
(T14)
(T15)
(T13)
(T8)
(T6)
(T7)
(T5)
(T4)
(T2)
(T3)
(T1)
(T12)
(T10)
(T11)
(T9)
Bottom Left Panel
Bottom Right Panel
TopLeft Panel
TopRight Panel
1A 4A
3A 6A 6B
4B1B
3B
2
5
N2N2
(P) (T
)(T)
(P)Fill and Drain ValveFlow Control Valve Normally ClosedFlow Control Valve Normally OpenFilterThrust Chamber Valve (TCV)Valve Branch AValve Branch BHeaterPressureTemperatureThrusterIsolation ValvePressure RegulatorRelief Valve
(P)(T)
R1 R2 R3 R4