Specs.pdf

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High pressure water pump for stand 2 in ASCR. Federal contract opportunity
Solicitation number
80NSSC19Q1022
Issued by
National Aeronautics and Space Administration Shared Services Center

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RFQ_80NSSC19Q1022.pdf PDF

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NASA Glenn Research Center Probe Cooling Water Pump Specifications

Advanced Subsonic Combustion Rig (ASCR) Water Coolant Pump

Technical Requirements Minimum Specification

1 Fluid 10-micron filtered domestic non potable softened water between 50°F – 80°F 2 Type Horizontal Centrifugal, motor and pump assembly non-pulsating 3 Pump Capacity 30-gpm 4 Suction Pressure Gravity Fed 5 Discharge Pressure 1500-psig 6 Suction Connection 3” ASME B16.5 class 7 Discharge Connection 2” ASME B16.5 class flange 8 Electrical Motor 3Φ; 460 VAC; 60 Hz; minimum Class I, Div II, Group D explosion proof motor rated for 200°C or less 9 Motor/Pump Footprint 9 feet long x 4 feet wide x 3 feet high maximum dimensions 10 Pump Curve Two hard copies and an electronic version 11 Installation instructions Two hard copies and electronic version 12 Maintenance Manual Two hard copies and an electronic version 13 Rebuild Manual Two hard copies and an electronic version 14 Pump Standby Guidelines Two hard copies and an electronic version 15 Recommended Spare Part List Two hard copies and an electronic version 16 Technical Support On-site installation assistance, oversight and service rep availability if needed 17 Performance History Pump model or variations of the same model that has been on the market for more than five years 18 Drain Low point ports on pump casing for draining during long periods of down time 19 Vent High point vent port for removing entrained air 20 Minimum Filtration Filtration requirements ten micron or greater 21 Extended Storage Pumps shall be capable of non-operational periods for up to one year when they are installed

Better Value Features

1. Delivery timeframe of less than 16-weeks after contract award

2. Minimum recommended service cycle based on proposed model’s historical history

3. In support of the NASA “Buy-Quiet” goal, pumps shall emit noise levels as low as feasibly possible, with a target criteria of an A-weighted noise emission less than 85dB (A), as an A-weighted sound level measured at 1 meter during all operational states of the pump and motor. Impulse sound pressure levels should not exceed 130 dB LPC, peak at any designated measurement location and at the operator’s ear, during operation of the machine. Simplified technical guidance for measurement of sound level emissions can be found on the NASA buyquietroadmap.com website:

http://buyquietroadmap.com/wp-content/uploads/2010/02/Field-Verification.pdf.

a. The criterion applies to equipment operation at no load and under all anticipated and actual production loads under final installed conditions, including noise associated with the material handling, as applicable.

b. An equipment system consisting of multiple components (e.g., motor, gearbox and pump combination) shall comply with the criterion as a complete system rather than as individual components.

c. Sound control treatments shall be designed to permit access to equipment for operations and maintenance. These treatment designs shall not interfere with safety or reliability.

Acceptance Criteria

Cost Technical Pump past performance

Delivery

Delivery no later than 16-weeks after contract award http://buyquietroadmap.com/wp-content/uploads/2010/02/Field-Verification.pdf

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