Attachment_0007_Integration_Schedule_Events.pdf

Attachment 0007

Integration Schedule Events

WBS

Element Task Evidence Standard Schedule

Duration

1.3.1.1 & 1.3.1.2

Multiplayer and

SWDAR

Modifications Design

Video format 720p HD-SDI or Analog NTSC 17 days

1.3.2.1 Payload Hardware

Integration Design Mechanical drawings Mechanical Interface compatible with

ICD Section 3.1.1 5 days

1.3.2.2 Encoder Modifications Design

Video format 720p HD-SDI or Analog NTSC 10 days

1.3.2.3 Payload INS Design Electrical interface

document GPS Interface per ICD Section 3.3.4 20 days

1.3.2.4 Electrical Harness

Design

Electrical interface drawing

Compatibility with existing wiring harness per ICD Section 3.4 10 days

1.3.2.6 Shock Mount

Design Mechanical Drawings

Compliance with mechanical installation utilizing no shock isolators per ICD Section 3.1.1, or utilizing shock isolators (NSN 5340-33-210- 7059) per ICD Section 3.1.2 if isolation is necessary.

5 days

1.3.2.8 Electromagnetic Environmental Effects (E3) Design

Test report

Documented operation while exposed to electromagnetic environments specified in PBS sections 3.9.5.2 and 3.9.5.3

5 days

1.7.5.4 Electromagnetic Environments Ground Testing

Test report

Documented operation while exposed to electromagnetic environments specified in PBS sections 3.9.5.2 and 3.9.5.3

5 days

1.7.5.7 Public Health

Command Testing

Laser subsystem functional design documentation

Compliance with PBS Sections

3.4.1.3.1 (LTM States), 3.4.1.4.1 (LRF States), 3.4.1.5.1 (LD States)

20 days

1.7.5.8 Hellfire Verification

Testing

Laser subsystem functional design documentation

Compliance with PBS Sections

3.4.1.3.1 (LTM States), 3.4.1.4.1 (LRF States), 3.4.1.5.1 (LD States)

15 days

1.7.5.12 GPS Testing Test report Documentation of integration on an aircraft that uses SAASM GPS 5 days