SOLICITATION NOTICE
66 -- FUSED SILICA WINDOW
- Notice Date
- 5/13/2015
- Notice Type
- Combined Synopsis/Solicitation
- NAICS
- 333314
— Optical Instrument and Lens Manufacturing
- Contracting Office
- NASA/Goddard Space Flight Center, Code 210.Y, Greenbelt, MD 20771
- ZIP Code
- 20771
- Solicitation Number
- NNG15547978Q
- Response Due
- 5/21/2015
- Archive Date
- 5/13/2016
- Point of Contact
- MONICA DELORESS REESE, PURCHASING AGENT, Phone 301-286-4920, Fax 301-286-5373, Email MONICA.REESE@NASA.GOV
- E-Mail Address
-
MONICA DELORESS REESE
(MONICA.REESE@NASA.GOV)
- Small Business Set-Aside
- N/A
- Description
- NASA/GSFC has a requirement for Window 1 NOT ITAR Quantity 2 1. Material: Fused Silica - Corning 7980 0F grade (or equivalent) 2. Diameter: 304.8 mm + 0.0 mm/ -0.5 3. Thickness: 25.0 mm +/- 0.3 mm (low side of wedge) 4. Wedge: less than 1 min. 5. Transmitted wavefront error: /= 285 mm 7. Surface quality within clear aperture shall be 60-40 IAW mil-prf-13830b as applied to scratches and digs. 8. Chamfer edges 0.5 mm minimum face width, 1.5 mm maximum 9. Edge chip width not to exceed 0.5 mm intrusion of polished surface from chamfer edge. Total length of edge chips not to exceed 5% of perimeter. All visible edge chips shall be stoned or polished smooth. 10. Fine grind all non-optical surfaces 11. Anti-reflection coat clear apertures of surfaces s1 and s2 as follows: A. Wavelengths: 0.355, 0.532, 0.775, 1.064 and 1.550 microns B. The coatings shall withstand exposure to the humidity, salt spray fog, moderate abrasion, and adhesion tests of mil-prf-13830b in the sequence listed herein and shall conform to the requirements of section c.3.4 (coating quality), c.3.4.1 (physical), c.3.4.3 (spatter and holes), and c.3.4.4 (surface defects scratch and dig). C. Transmittance, environmental, and durability tests may be performed on a witness sample not less than 1 inch in diameter and 0.040 inch thick of the same material and coated with the deliverable hardware. The reflectance sample may be a like part which has been rejected for reasons not affecting the coating. D. Transmittance and reflectance traces and one witness sample to accompany the hardware from each coating run. E. The material used in the manufacture of these coatings shall not contain thorium or other radioactive materials. F. Average reflectance per surface < 1.0% at wavelengths specified for normal incidence. G. Coating shall withstand cleaning with reagent grade ethanol, methanol, acetone, or distilled water. 12. Each delivered part shall be accompanied with the following: A. Spectral reflectance and transmittance curves showing compliance with note 11. A. Spectral reflectance and transmittance curves showing compliance with note 11. B. All witness samples used for verification of note 11 requirements. C. Copies of test reports showing actual measured values verifying all dimensions and compliance with all drawing requirements for each part delivered. D. Certification of material compliance 13. Temperature performance A. Operational: all of the requirements specified herein shall be met over a temperature range of 10 to +30 Degrees C B. Storage: all of the requirements specified herein shall be met after exposure to temperatures within the Range of 40 to +71 degrees C Window 2 NOT ITAR Quantity 1 1. Material: Fused Silica - Corning 7980 0F grade (or equivalent) 2. Diameter: 355.6 mm + 0.0 mm/ -0.5 3. Thickness: 25.0 mm +/- 0.3 mm (low side of wedge) 4. Wedge: less than 1 min. 5. Transmitted wavefront error: /= 325 mm 7. Surface quality within clear aperture shall be 60-40 IAW mil-prf-13830b as applied to scratches and digs. 8. Chamfer edges 0.5 mm minimum face width, 1.5 mm maximum 9. Edge chip width not to exceed 0.5 mm intrusion of polished surface from chamfer edge. Total length of edge chips not to exceed 5% of perimeter. All visible edge chips shall be stoned or polished smooth. 10. Fine grind all non-optical surfaces 11. Anti-reflection coat clear apertures of surfaces s1 and s2 as follows: A. Wavelengths: 0.355, 0.532 and 1.064 microns B. The coatings shall withstand exposure to the humidity, salt spray fog, moderate abrasion, and adhesion tests of mil-prf-13830b in the sequence listed herein and shall conform to the requirements of section c.3.4 (coating quality), c.3.4.1 (physical), c.3.4.3 (spatter and holes), and c.3.4.4 (surface defects scratch and dig). C. Transmittance, environmental, and durability tests may be performed on a witness sample not less than 1 inch in diameter and 0.040 inch thick of the same material and coated with the deliverable hardware. The reflectance sample may be a like part which has been rejected for reasons not affecting the coating. D. Transmittance and reflectance traces and one witness sample to accompany the hardware from each coating run. E. The material used in the manufacture of these coatings shall not contain thorium or other radioactive materials. F. Average reflectance per surface < 1.5% at wavelengths specified for angles of incidence between 0 and 20 degrees G. Coating shall withstand cleaning with reagent grade ethanol, methanol, acetone, or distilled water. 12. Each delivered part shall be accompanied with the following: A. Spectral reflectance and transmittance curves showing compliance with note 11. B. All witness samples used for verification of note 11 requirements. C. Copies of test reports showing actual measured values verifying all dimensions and C. Copies of test reports showing actual measured values verifying all dimensions and compliance with all drawing requirements for each part delivered. D. Certification of material compliance 13. Temperature performance A. Operational: all of the requirements specified herein shall be met over a temperature range of 40 to +30 Degrees C B. Storage: all of the requirements specified herein shall be met after exposure to temperatures within the Range of 80 to +71 degrees C This notice is a combined synopsis/solicitation for commercial items prepared in accordance with the format in FAR Subpart 12.6, as supplemented with additional information included in this notice. This announcement constitutes the only solicitation, which is issued as a Request for Quotation (RFQ); quotes are being requested and a written solicitation will not be issued. Offerors are required to use the On-Line RFQ system to submit their quote. The On-line RFQ system is linked above or it may be accessed at http://prod.nais.nasa.g ov/cgi-bin/eps/bizops.cgi?gr=C&pin=. The information required by FAR Subpart 12.6 is included in the on-line RFQ. The Government intends to acquire a commercial item using FAR Part 12 and the Simplified Acquisition Procedures set forth in FAR Part 13. Questions regarding this acquisition must be submitted in writing (e-mail is preferred) no later than May 18, 2015. It is the quoter's responsibility to monitor this site for the release of amendments (if any). Potential quoters will be responsible for downloading their own copy of this notice, the on-line RFQ and amendments (if any). NASA Clause 1852.215-84, Ombudsman, is applicable. The Center Ombudsman for this acquisition can be found at http://prod.nais.nasa.gov/pub/p ub_library/Omb.html.
- Web Link
-
FBO.gov Permalink
(https://www.fbo.gov/spg/NASA/GSFC/OPDC20220/NNG15547978Q/listing.html)
- Record
- SN03729569-W 20150515/150513234749-86ca058c574e125a33b621acb3b34965 (fbodaily.com)
- Source
-
FedBizOpps Link to This Notice
(may not be valid after Archive Date)
| FSG Index | This Issue's Index | Today's FBO Daily Index Page |