Pricing_Worksheet.doc

DOC document 35 KB Posted

Attached to
Gyro-Stabilized Positioning System Federal contract opportunity
Solicitation number
FA2823-17-Q-0073
Issued by
Department of the Air Force Materiel Command Test Center

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Class_Deviation_2012-O0004.pdf PDF
COMBO_Stabilized_Positioning_System.pdf PDF
Positioning_System_TRD.pdf PDF

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Attachment 1

The following items will be procured:

CLIN
Part Number
Description
Qty
Unit Price
Extended Price

Gyro-Stabilized Positioning System:

FOB Destination
1

Shipping

Total

CLIN 0001 – Gyro-Stabilized Positioning System:

a. 2-axis, elevation over azimuth platform

b. Line-of-sight stabilization

c. Position Resolution: 3 µradians

d. Position Accuracy: +/- 100 µradians

e. Payload up to 150 lbs.

f. Azimuth Travel: +/- 175°

g. Elevation Travel: -15° to +95°

h. Speed: up to 90°/sec

i. Acceleration: up to 90°/sec2

j. Stow locks for travel

k. Operating Temperature: -30°C to +55°C

Mechanical

a. Yoke-style configuration

b. Payload mounting surface: at least 16” perpendicular to line-of-sight x 8” along line-of-sight

c. Positioner Weight ≤ 90 lbs.

Electrical

a. Control Interface: RS-232/422 or Ethernet, ICD or SDK provided

b. Power: 115 VAC, 60 Hz

Control Interface

a. Provide system status updates (Azimuth, Elevation, Rates at minimum) available at a minimum of 30Hz

b. Accept system status updates of at least 30Hz

CLIN 0002 – Freight On Board Destination

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