1a.__STATEMENT_OF_REQUIREMENTS.pdf

STATEMENT OF REQUIREMENTS

For NASA Kennedy Space Center 5-Axis Gyro-Stabilized Gimbal Camera System

Objective: The purpose of this Statement of Requirements is to provide the requirements for a NASA Kennedy Space Center EGS 5-axis gyro-stabilized gimbal camera system.

Delivery Date: No later than 90 days after receipt of order or May 31, 2018, whichever is earliest

Scope of Work: Provide NASA KSC with 5-axis gyro-stabilized gimbal camera system that meets camera description, specifications and capabilities identified below.

Camera Description: Single payload capability and interchangeability between two or more camera systems.

Camera Specifications: Capability of controlling unit from at least 80 feet away from system using hardwired controller with full pan, tilt, zoom and focus controls.

Ability to attain airworthiness.

Must operate up to 25,000 feet PA. Desired operation up to 35,000 feet PA.

Ability to operate in temperatures 0° to +120° Fahrenheit Sealed system to prevent water/rain/moisture from inside of unit Gimbal unit must be able to work in both standard and inverted configurations Ability to operate 360° continuous spin Ability to change camera/lens payloads in the field in less than 2 hours No ITAR/EAR export restrictions.

Provide estimated product life cycle (years of service).

Include ability to integrate B4 lens onto PL camera mount (IB/E HDx35 MKII B4/PL Optical Adapter) Ability to operate up to 200 knots air speed Ability to integrate listed camera hardware systems:

- Camera o Red Weapon 8K Helium o Red Epic 6K Dragon o Arri Alexa Mini o Canon C700

- Lens Options o Canon 50-1000mm (w/ 2x teleconverter) o Angenieux 40x11 o Canon HJ40x14B

Include system shipping cases (ability to be included as excess baggage)