Light Weight, Scalable Manufacturing of Telescope Optics

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX13CM21P
Agency Tracking Number: 124554
Amount: $124,626.00
Phase: Phase I
Program: SBIR
Awards Year: 2013
Solicitation Year: 2012
Solicitation Topic Code: S2.04
Solicitation Number: N/A
Small Business Information
NY, Stony Brook, NY, 11790-3350
DUNS: 830864448
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Christopher Jensen
 Senior Project Engineer
 (631) 739-8818
Business Contact
 Wanhuk Choi
Title: Chief Operating Officer
Phone: (631) 739-8818
Research Institution
NASA's future X-ray astronomy missions will require X-ray optics that have large effective areas, are lightweight, and cost effective. Recent X-ray telescopes, such as the Chandra Observatory, utilized reflectors made from zerodur which were up to 20mm thick. The thickness of the reflector as well as the mass limited the number of nested optics that could be implemented. The current state of the art reflectors are made from electroformed nickel/cobalt which is on the order of 1mm thick. The implementation of these thin optics have greatly increased the number of nested reflectors possible. XMM-Newton uses such optics and consists of 58 nested reflectors compared to 4 for Chandra.Aside from the manufacturing cost of the reflectors themselves, the mass of the telescope is a large factor that determines the overall cost of the mission, mainly due to the requirements of the launch vehicle. The proposed innovation seeks to improve upon the current state of the art by replacing much of the NiCo with a stiff, lightweight ceramic material. A thermal spray process will be developed to allow for the deposition of porosity graded alumina onto the rear surface of the reflector. Several diagnostic techniques will be used to adjust the inflight particle state as well as the resulting residual stress of the coating as to not adversely affect the figure accuracy of the optic. The gradation of the alumina layer will allow for CTE matching with the electroformed shell as well as optimization of the ceramic stiffness.By reducing the NiCo layer from 1mm to less than 100um and adding a 200um alumina layer as the support structure the overall mass of the telescope can be greatly reduced and thus reduce the overall cost of the mission. Additionally the overall thinner optic would allow a greater packing density and increase the capabilities of such X-ray telescopes.

* Information listed above is at the time of submission. *

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