B08_Salients_Camera_Enclosure_revised_8_1_23.pdf
PDF 135 KB Posted
- Attached to
- AERIAL CAMERA POD and ACCESSORIES IAW SOW
- Solicitation number
- 140G0123Q0243
About this file
This statement of work describes requirements for an aerial camera pod enclosure. The U.S. Geological Survey needs a custom-built sensor enclosure compatible with a Cessna 182 aircraft. The enclosure must house a Lucint M multispectral camera measuring 4.125 x 4.125 x 2.65 inches. It must integrate with a Meeker Aviation strut mount and quick release, accommodate the camera in nadir or oblique orientation, and include customized antivibration mounts. The selected vendor will integrate the camera into the enclosure, designing mounting brackets, vibration isolators, and openings. A travel case is also required. The related solicitation is for this aerial camera pod and accessories per the statement of work. Offerors should respond to solicitation number 140G0123Q0243 issued by the Department of the Interior US Geological Survey Office of Acquisitions and Grants.
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Other files
| File | Type | Posted |
|---|---|---|
| B09_ATCH_2_SALIENTS_Camera_Enclosure_Part_2_08-11-2023_0001.pdf | ||
| Sol_140G0123Q0243_Amd_0001.pdf | ||
| Sol_140G0123Q0243.pdf |
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Text version
AERIAL CAMERA POD
1.0 INTRODUCTION AND BACKGROUND
The U.S. Geological Survey, Water Mission Area, Observing Systems Division, Hydrologic Remote Sensing
Branch (HRSB) needs to procure a sensor enclosure with sufficient volume and flexibility to house a multispectral camera system. The sensor enclosure will be used to collect aerial remote sensing data from a Cessna 182 aircraft. This Statement of Work (SOW) describes the government’s requirements.
The enclosure will be custom built.
2.0 SCOPE
This SOW is for a sensor enclosure with the ability to house a multispectral camera from Lucint (model
Lucint‐M). The physical dimensions of the multispectral camera payload are 4.125 in x 4.125 in x 2.65 in
(excluding lenses). The enclosure must be compatible with a Meeker Aviation strut mount and dovetail quick release designed and approved for a Cessna 182 aircraft. The enclosure must be able to accommodate the camera payload in either an oblique or nadir orientation. The enclosure must have customized anti‐vibration mounts that can be customized for the weight and center of gravity for the camera payload. The vendor will integrate the multispectral camera payload supplied by the USGS HRSB, with the enclosure. Integration includes the design of enclosure mounting brackets, vibration isolators, and hole openings. A travel case for shipping the enclosure will also be included.
3.0 APPLICABLE DOCUMENTS ‐ NA
4.0 TECHNICAL REQUIREMENTS
A. Aircraft Make and Model Requirements and Approvals
Sensor enclosure will be compatible with Meeker strut mount (AFWM‐182‐1/‐2) and quick release (DT‐1‐1) designed for Cessna 182 by Meeker Aviation
Sensor enclosure must be able to accommodate payload in either oblique or nadir orientation
B. Physical and Environmental Specifications of Sensor Enclosure:
• Length < 30 inches without antenna mount, Width < 15 inches, Height < 15 inches
• Empty weight < 20 lbs.
• Volume > 2000 cubic inches
• Water resistant housing ‐the top portion of the housing is made from aluminum and the bottom portion from plastic.
5.0 DELIVERABLES
Sensor enclosure including necessary mounting brackets, vibration isolators, and hole openings for integration
Shipping case
Delivery Date: Two weeks after award or September 1, 2023, whichever date is sooner
Delivery Address: U.S. Geological Survey, 4620 Technology Drive, Suite 400, Golden, CO 80403
File details come from the government source that posted it. Updated .