SOURCES SOUGHT
66 -- PRESSURE TRANSDUCER
- Notice Date
- 7/17/2012
- Notice Type
- Sources Sought
- NAICS
- 334519
— Other Measuring and Controlling Device Manufacturing
- Contracting Office
- NASA/John F. Kennedy Space Center, Procurement, Kennedy Space Center, FL 32899
- ZIP Code
- 32899
- Solicitation Number
- NNK12CZ006R
- Response Due
- 8/1/2012
- Archive Date
- 7/17/2013
- Point of Contact
- A. Zuber Christopher, Contract Specialist, Phone 321-867-2115, Fax 321-867-1166, Email Christopher.Zuber@nasa.gov
- E-Mail Address
-
A. Zuber Christopher
(Christopher.Zuber@nasa.gov)
- Small Business Set-Aside
- N/A
- Description
- NASA/KSC is hereby soliciting information about potential sources for light-weight low power pressure transducers for operation in in a thermal vacuum chamber. The National Aeronautics and Space Administration (NASA) Kennedy Space Center is seeking capability statements from all interested parties, including Small, Small Disadvantaged (SDB), 8(a), Woman-owned (WOSB), Veteran Owned (VOSB), Service Disabled Veteran Owned (SD-VOSB), Historically Underutilized Business Zone (HUBZone) businesses, and Historically Black Colleges and Universities (HBCU)/Minority Institutions (MI) for the purposes of determining the appropriate level of competition and/or small business subcontracting goals for pressure transducers. The Government reserves the right to consider a Small, 8(a), Woman-owned (WOSB), Service Disabled Veteran (SD-VOSB), or HUBZone business set-aside based on responses hereto. 1. Background and Plan NASA/KSC is currently studying the feasibility, practicality, and cost of developing light-weight low-power pressure transducers to be utilized within the Regolith and Environment Science and Oxygen and Lunar Volatile Extraction (RESOLVE) project's Lunar Advanced Volatile Analysis (LAVA) Subsystem to make decisions regarding procurement strategies for the development of instrumentation. RESOLVE is a lunar resource prospecting payload that is in development for a launch opportunity to the Moon. 2. Technical Requirements: The pressure transducers sought in this announcement will be used to measure gas pressure in the LAVA fluid system composed of 1/8in and 1/16in tubing, a fluid manifold (flat surface), a tank (round surface), a gas chromatograph / mass spectrometer (GC-MS) instrument, and three small high-pressure gas cylinders. There are three operating regimes for these pressure transducers: The first operating regime requires measurement of pressure for two small high-pressure gas cylinders, including Hydrogen up to 2200 psi and a carrier gas up to 2200 psi. These pressure transducers will be required to be mounted on a manifold with 1/8in fluid lines. NASA anticipates the acquisition of six (6) units. The second operating regime requires measurement of pressure for a small high-pressure gas cylinder of calibration gas up to 500 psi. These pressure transducers will be required to be mounted on a manifold with 1/8in fluid lines. NASA anticipates the acquisition of three (3) units. The third operating regime requires measurement of pressure from 0 to 100 psi. These pressure transducers will be required to be mounted on a manifold with 1/8in fluid lines. NASA anticipates the acquisition of nine (9) units. All pressure transducers must operate using an 18-36 VDC power supply. The pressure transducers shall utilize no more than 1 Watt per unit. The pressure transducers shall be capable of operating in the ranges of 0 to 2200 psi for the first regime, 0 to 500 psi for the second regime, and 0 to 100 psi for the third regime. Pressure transducers operating in the 0 to 100 psi regime shall measure pressure in the fluid system to within +/- 0.5 psia accuracy. All other pressure transducers shall measure pressure in the fluid system to within 0.2% FS accuracy. The vendor must specify the accuracy the pressure transducer can achieve. The pressure transducers must operate within specification in a temperature environment of -20C to 175C in an external ambient pressure as low as 10^(-10) Torr. The mass for each pressure transducer in the lower pressure (up to 100 psi) regime shall not exceed 35 grams. The vendor must specify the mass of each pressure transducer. The pressure transducer signal response delay must be less than 100 milliseconds. All pressure transducers will be required to operate and maintain integrity after exposure to temperatures ranging from -30C to 200C (the pressure transducers will not be required to operate under these conditions, but must survive and operate after being exposed to these temperature conditions). The desired mean-time between failures is estimated to be 5,000 hours with a minimum lifetime of 10,000 hours. The gases in the fluid system will consist of either pure hydrogen or a mixture of various gases consisting mainly of hydrogen, water vapor, and low concentrations of other gases such as carbon monoxide, hydrochloric acid, hydrofluoric acid, and hydrogen sulfide. All pressure transducers, except for that used near the Hydrogen cylinder, shall be limited to 100 or less hours of exposure to pure Hydrogen. The fluid system is being designed to make quantitative measurements of water; therefore, material selection for the pressure transducer components in contact with the fluid must not absorb water, nor be a source of other volatiles (off-gassing). Also, short-duration exposure (30min) to small amounts (<1%) of hydrofluoric acid and hydrochloric acid are expected. All wetted materials shall be inert. The vendor shall indicate any flight heritage or if any flight qualification testing has been performed. 3. Additional Information a. Commercial off-the-shelf (COTS) products are desired with associated cost per item to establish a reasonable target cost for developing and qualifying these components that meets the requirements defined. Please advise if the requirement is considered to be a commercial or commercial-type product. A commercial item is defined in FAR 2.101. If modified COTS items can be designed to meet these requirements, please include the following: i. Rough Order of Magnitude (ROM) cost estimate for Developmental units with non- recurring engineering (NRE). ii. Rough Order of Magnitude (ROM) cost estimate of subsequent production units. iii. Estimated delivery/lead time for first three (3) units. iv. Estimated delivery/lead time for six (6) production units. RFI Questions: NASA is requesting responses to the following questions: Pressure Transducer Capabilities: 1. Would your organization be interested in developing pressure transducers for NASA missions? 2. What experience with pressure transducers do you have? (a) Airborne or space flight applications (b) Reliability requirements and performance of current products; (c) Current pressure transducer use/applications; brief description of pressure transducer requirements including operational life (d) Years of pressure transducer manufacturing and production experience (e) What related heritage programs have you previously worked on, and at what scope (Prime Supplier, subcontractor, etc)? 3. From your perspective, what will be the major technical risks in developing pressure transducers that meet the specifications provided? Questions and comments are welcomed. All questions regarding and correspondence associated with this RFI should be conducted by email. The NAICS code for this requirement is 334519 with a size standard of 500 employees. The government does intend to acquire a commercial item using FAR Part 12. No solicitation exists; therefore, do not request a copy of the solicitation. If a solicitation is released it will be synopsized in FedBizOpps and on the NASA Acquisition Internet Service. It is the potential offerors responsibility to monitor these sites for the release of any solicitation or synopsis. Interested offerors/vendors having the required specialized capabilities to meet the above requirement should submit a capability statement of five (5) pages or less indicating the ability to perform all aspects of the effort described herein. Respondents are required to address the following technical specifications for their respective pressure transducer designs. Responses must have classified and proprietary information properly marked. For planning purposes, we are requesting that the responses to this RFI include the following information at a minimum: Brief description of company capabilities, applicable facilities, and experience designing pressure transducers. Description of previous flight heritage and pressure transducer concept using the stated specifications as the basis Notional schedule for development, testing and qualification through delivery based on your approach, technology maturity and understanding of the risks. Assume ten (18) units to be delivered. Twelve (12) qualification units by May 2013 and six (6) flight units in 2014. Description of key technical, schedule, and cost drivers and options to mitigate risks and/or reduce schedule To facilitate a prompt review by the NASA team, a one (1) page summary shall be included with your capability statement(s), identifying the following information: 1. Company name and address. 2. Contractor size/type classification (Large, Small, Small Disadvantaged 8(a), Woman-Owned, Veteran-Owned, Service Disabled Veteran and HUBZone). 3. Company size (number of employees). 4. Average annual revenue for the past three (3) years. 5. Affiliate information (as applicable) including, parent company, joint venture partners, prime contractor (if potential sub) or subcontractors (if potential prime), point of contact name, position, address and phone number. 6. Company specific capabilities that are relevant to the requirements listed above. It is not sufficient to provide only general brochures or generic information. Copies of your capability statement(s) may be made available to prospective offerors in the future. Therefore, it should not contain company-sensitive information, This synopsis is for information and planning purposes and is not to be construed as a commitment by the Government nor will the Government pay for information solicited. Respondents will not be notified of the results of the evaluation. Respondents deemed fully qualified will be considered in any resultant solicitation for the requirement. All responses shall be submitted electronically to Chris Zuber at Christopher.Zuber@nasa.gov no later than August 1, 2012. Please reference NNK12CZ006R in any response. Any referenced notes may be viewed at the following URLs linked below.
- Web Link
-
FBO.gov Permalink
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- Record
- SN02805751-W 20120719/120718000129-23527d584bfebefb78cfa080cb245a2f (fbodaily.com)
- Source
-
FedBizOpps Link to This Notice
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