Product_Description_and_Specification_-_ICP.pdf

PURCHASE DESCRIPTION

FOR

Inductively Coupled Plasma Optical Emission Spectrometer

809 MXSS

24 May 2018

809 MXSS/MXDTAB

7278 4th STREET

BLDG. 100, BAY D

ATTN: Mitch Smolcha

HILL AFB UT 84056

1.0. DESCRIPTION OF REQUIREMENTS

The Chemical Flight within the 809th Maintenance Support Squadron (Science and Engineering Lab) is required to purchase an Inductively Coupled Plasma Optical Emission Spectrometer (ICP-

OES) located in building 100 Bay E. The ICP-OES must have axial and radial view capability in the same instrument, have a CCD detector, contain a Rowland Circle optical system with argon purged chamber and have an internal air based cooling system.

1.1. ACCESSORIES AND SPECIFICATIONS

The ICP-OES system must meet the following specifications and possess the following capabilities:

Polychromator

Thermally stabilized to +15%˚C ± 0.5 ˚C

750 mm focal length

Holographic concave master grating: 2 x 3600 grooves/mm, 1 x 1800 g/mm

Grating material Zerodur

MgF2 optical components

Full 1st order wavelength coverage

Wavelength range: 130 (160)1 – 770 nm

Entrance slits width: 15 µm

Detector

32(29)1 linear CCD arrays, fitted continuous order, selected and optimized according to the wavelength range

3648 pixels per array

Optical/pixel resolution: 130 (160)1 – 340 nm 8.5 pm/3 pm, >340 nm 16pm/6pm

Thermally stabilized optical system

Parallel readout architecture

0.75M Roland Circle optical system capable of a resolution of 0.008nm.

On board digital signal processor for each CCD array

Intelligent data acquisition and data reduction system

Dynamic range up to 9 orders of magnitude

Shortest integration time 0.1 ms

Shortest measurement time for one analysis 2 sec

Integration time automatically optimized for each pixel according to signal height

Full spectrum access

Automatic dark current correction

Automatic profile standardization

TCP/IP interface to data processing system

UV System

Gas(Argon) filled hollow section, sealed, no consumable purge gas required

Dual Window entrance optics, easy to maintain

Automatic gas purifying system

Purifying cartridge lifetime 24 months

RF-Generator

LDMOS solid state design

Frequency: 27.12 MHz free running type

RF power output: 0.5 to 2.0 kW

Power efficiency >85%

Automatic plasma ignition

Stand by mode

Fully computer controlled

Air Cooled (No external cooling required)

Sample Introduction System and Torch Unit

Bayonet, single turn mount component holder

Gas connections included in the torch body

Thermostatically insulated sample introduction area

Integrated 70 speed, 4 channel, 12 roller, computer controlled peristaltic pump

Fast pre flush and fast rinse function

Peristaltic pump drain

Multi view instrument…true axial and true radial plasma observation capability

PC System with minimum Intel Dual Core 3.10 GHz processor, 4GB Ram, 500 GB HD, Color LCD Monitor and Laser Printer, Windows 10 and sample processing software compatible with Windows 10

Spectrometer maximum dimensions: (42.1 x 62.3 x 29.8 in)

Footprint maximum: (41.9 x 25.4 in)

Weight: no more than 530 lbs

1.2. CONTRACTUAL REQUIREMENTS

1.2.1. Delivery

The contractor shall deliver the equipment to the following address located at Hill Air Force Base:

809 MXSS/MXDTAB

7278 4th Street Bldg. 100, Bay D Attn: Greg Hardcastle Hill AFB UT 84056-5825

1.2.2. Training and Installation:

The system must be installed by qualified factory trained service engineer(s) directly employed by the vendor. Method creation, basic operation and instrument service/maintenance training, for a minimum of 2 operators, must be provided by the installing engineer upon completion of installation.

All labor, food, travel and accommodation expenses for the service engineer(s) and applications specialist(s) shall be included in proposal.

1.2.3. Warranty

The contractor shall provide a minimum 1 year warranty which warrants all products provided under this contract, under normal use, free from defects in materials and workmanship and that system will perform its design function for a period of no less than one (1) year. Warranty period to start from date of final acceptance of each installed unit/system. Any defects in materials or workmanship or failure of any product or component to perform its designed function during the warranty period shall be fixed by the contactor at no additional cost to the government. Warranty shall include the cost(s) of, parts, shipping, labor and any travel related expenses. Warranty repairs which present a safety hazard are to be repaired within 7 calendar days of notice of failure. Non-safety related warranty repairs are to be fixed within 15 calendar days of notice of failure.