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CONOPS

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02/24/2004 Proposed Possible Tasks Evaluation & Certification Standardizing the system System Modification Enhance support capabilities Sealing Cargo Hold ... – PowerPoint PPT presentation

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Title: CONOPS


1
02/24/2004
2
CONOPS
3
(No Transcript)
4
Major Design Constraints and Considerations
  • No aircraft modification
  • C-130 minimal mission interference
  • C4ISR Command, Control, Communications,
    Computers, Intelligence, Surveillance and
    Reconnaissance
  • Multi-mission flexibility (Counter Drug,
    Environmental Impact Assessment, Counter
    Terrorism, HLS, Resource Surveys, Environmental
    Surveys)
  • GOTS and COTS
  • Ground-to-air deployment
  • (lt 2 hours)

5
Major Design Constraints and Considerations
cont.
  • Upgrade flexibility
  • In-flight deployable
  • Adequate space for various sensor configuration
  • Standardized mounting/ connection of systems
  • Power usage supplied within limits of C-130
  • Platform Stability

6
Standardized C-130 Pallet
7
C-130 Fuselage
Operator Station
Sensor Platform
8
Sensor Platform
9
Sensor Platform
10
Sensor Platform
Sensor Platform Rail System Major Components
  • Linear Actuator (manual and automatic control)
  • Rotational Gear Motor (manual and automatic
    control)
  • Mechanical Arm/Pod System
  • Proximity Sensors (linear and rotational
    control)

11
Sensor Platform Assembly
12
Loading Sensor Pallet
Securing Sensor Pallet
13
Deployment Process
  • Linear Translation (18 inches) - 20 seconds
  • Rotational Movement (237) - 15 seconds
  • Linear Retraction (12 inches) - 15 seconds
  • Complete Deployment - lt 60 seconds

14
Deployment Process
Mechanical Arm and Pod Incremental Articulation

15
Deployment Process
Leaving Stowed Position
Closing Deployed Position -
16
Mechanical Arm and Pod FEA
Analysis
  • Restraints set along shaft supports
  • Forces applied simulating drag
  • Material type/thickness selection

17
Operator Station
18
Operator Station
19
Operator Station
Loading Operator Station
Operator Station in Cargo-Hold
20
Operator Station
Components
  • 2 computer stations
  • 3 electronic racks
  • Climate control (Fan and vent unit, dehumidifier)
  • Communication panels
  • Power rectification
  • Direct or indirect lighting
  • 2 operator seats, 1 observer seat
  • 2 operator doors
  • Slingable/Stackable box

21
Operator Station
Powered Operator Station
Controls
22
Operator Station
Proposed Capabilities
  • Sensor operation/control
  • Data acquisition/interpretation
  • Data storage
  • Direct ground/ aircraft/ satellite communication
  • Converter for power supply
  • C4ISR Command, Control, Communications,
    Computers, Intelligence, Surveillance and
    Reconnaissance

23
Operator Station
Power Connection
Sensor Connection
24
Operator Station
Power Controller (rack mounted)
25
Sensor Pallet Electrical Layout
26
C-130 Power Distribution
27
C-130 Power Distribution
Close-up Power Distribution
28
Sensor Pallet Control
29
Sensor Pallet Control Pendant
30
GPS Communication
31
Aerodynamic Test
32
Aerodynamic Test
Pressure rake test
  • Air Test conducted on 02/04/2004 based on
    developed test matrix
  • Currently reducing data
  • Will compare data with that of simulation

33
Year Two
34
Proposed Possible Tasks
  • Evaluation Certification Standardizing the
    system
  • System Modification Enhance support
    capabilities
  • Sealing Cargo Hold Operate above 10,000 feet

35
As of 02/24/2004
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