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  • Instrumentation and Photography  (17)
  • Space Sciences (General)  (15)
  • 1
    Publication Date: 2019-09-26
    Description: HabEx is a space-based 4-meter diameter telescope with ultraviolet (UV), optical, and near-infrared (near-IR) imaging and spectroscopy capabilities. Three driving science goals during its five-year primary mission: 1. To seek out nearby worlds and explore their habitability.; 2. To map out nearby planetary systems and understand the diversity of the worlds they contain.; 3. To carry out observations that open up new windows on the universe from the UV through near-IR.
    Keywords: Space Sciences (General)
    Type: MSFC-E-DAA-TN60372 , MSFC-E-DAA-TN59966 , MSFC-E-DAA-TN72296 , SPIE Optics and Photonics; Aug 19, 2018 - Aug 23, 2018; San Diego, CA; United States|European Planetary Science Congress and Division for Planetary Science (EPSC-DPS) Meeting 2019; Sep 15, 2019 - Sep 20, 2019; Geneva; Switzerland
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  • 2
    Publication Date: 2019-07-12
    Description: At 2015 SPIE O&P we presented "Preliminary Analysis of Random Segment Errors on Coronagraph Performance" Key Findings: Contrast Leakage for 4thorder Sinc2(X) coronagraph is 10X more sensitive to random segment piston than random tip/tilt, Fewer segments (i.e. 1 ring) or very many segments (〉 16 rings) has less contrast leakage as a function of piston or tip/tilt than an aperture with 2 to 4 rings of segments. Revised Findings: Piston is only 2.5X more sensitive than Tip/Tilt
    Keywords: Instrumentation and Photography
    Type: MSFC-E-DAA-TN32194
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  • 3
    Publication Date: 2018-06-12
    Description: Scheduled to begin its 10 year mission no sooner than 2013, the James Webb Space Telescope (JWST) will search for the first luminous objects of the Universe to help answer fundamental questions about how the Universe came to look like it does today. At 6.5 meters in diameter, JWST will be the world's largest space telescope. This talk reviews science objectives for JWST and how they drive the JWST architecture, e.g. aperture, wavelength range and operating temperature. Additionally, the talk provides an overview of the JWST primary mirror technology development and fabrication status.
    Keywords: Instrumentation and Photography
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  • 4
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    In:  CASI
    Publication Date: 2019-07-20
    Description: The Habitable Exoplanet Observatory Mission (HabEx) will image and spectroscopically characterize planetary systems in the habitable zone around nearby sun-like stars. Additionally, HabEx will perform a broad range of general astrophysics science enabled by 100 to 2500 nm spectral range and 3 x 3 arc-minute FOV. Critical to achieving the HabEx science goals is a large, ultra-stable telescope. The baseline HabEx telescope is a 4-m off-axis unobscured three-mirror-anastigmatic design with diffraction limited performance at 400 nm and wavefront stability of picometers per mK. These specifications are driven by science requirements. STOP (structural thermal optical performance) analysis predicts that the baseline telescopes opto-mechanical design meets its specified performance tolerances.
    Keywords: Space Sciences (General)
    Type: MSFC-E-DAA-TN67198 , The Space Astrophysics Landscape for the 2020s and Beyond; Apr 01, 2019 - Apr 03, 2019; Potomac, MD; United States
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  • 5
    Publication Date: 2019-07-13
    Description: Technology advancement is required to enable NASA's high priority missions of the future. To prepare for those missions requires a roadmap of how to get from the current state of the art to where technology needs to be in 5, 10, 15 and 20 years. SIOSS identifies where substantial enhancements in mission capabilities are needed and provides strategic guidance for the agency's budget formulation and prioritization process.
    Keywords: Instrumentation and Photography
    Type: M11-1090 , NASA Cosmic Origins Program Analysis Group (COPAG) Meeting; Sep 22, 2011 - Sep 23, 2011; Baltimore, MD; United States
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  • 6
    Publication Date: 2019-07-12
    Description: The Advanced Technology Large-Aperture Space Telescope (ATLAST) is a concept for an 8-meter to 16-meter UVOIR space observatory for launch in the 2025-2030 era. ATLAST will allow astronomers to answer fundamental questions at the forefront of modern astrophysics, including "Is there life elsewhere in the Galaxy?" We present a range of science drivers that define the main performance requirements for ATLAST (8 to 16 milliarcsec angular resolution, diffraction limited imaging at 0.5 m wavelength, minimum collecting area of 45 square meters, high sensitivity to light wavelengths from 0.1 m to 2.4 m, high stability in wavefront sensing and control). We will also discuss the synergy between ATLAST and other anticipated future facilities (e.g., TMT, EELT, ALMA) and the priorities for technology development that will enable the construction for a cost that is comparable to current generation observatory-class space missions.
    Keywords: Instrumentation and Photography
    Type: GSFC.JA.5210.2011
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  • 7
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    In:  CASI
    Publication Date: 2019-07-19
    Description: Parametric cost models are an important tool for planning missions, compare concepts and justify technology investments. This paper presents on-going efforts to develop single variable and multi-variable cost models for space telescope optical telescope assembly (OTA). These models are based on data collected from historical space telescope missions. Standard statistical methods are used to derive CERs for OTA cost versus aperture diameter and mass. The results are compared with previously published models.
    Keywords: Instrumentation and Photography
    Type: M11-0380 , International Commission for Optics: (ICO) 22 General Congress; Aug 15, 2011 - Aug 19, 2011; Puebla; Mexico
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  • 8
    Publication Date: 2019-07-20
    Description: No abstract available
    Keywords: Space Sciences (General)
    Type: MSFC-E-DAA-TN64258 , Lecture at University of Alberta; Mar 20, 2019; Edmonton, Alberta; Canada
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  • 9
    Publication Date: 2019-07-13
    Description: Clean room standards like ISO 14644 used for facilities that construct spacecraft and store returned samples do not explicitly account for microbial contamination. While there are associated ISO standards for monitoring and controlling bio-contamination in clean rooms it is not always standard practice to do so. The NASA Astromaterials Acquisition and Curation Office maintains seven separate clean labs for storing extraterrestrial samples from the Moon, meteorites, cosmic dust, asteroids, comets, solar wind particles, and microparticle impact samples. These labs are routinely monitored for particulate and trace metal contamination. However, the sample collections are either non-sterile at the time of collection (e.g., meteorites) or are no longer being used to address scientific questions that could be affected by non-sterile conditions (e.g., Lunar samples). Outside of isolated studies there has not been a systematic, longitudinal characterization of the microbial ecology of NASA curation clean rooms. In accordance with the advanced curation initiative, and to prepare for future sample return missions, we have initiated a routine microbiological monitoring program in the Antarctic Meteorite Lab. This monitoring program will be used to determine what microbes are capable of surviving in these oligotrophic environments and whether or not they are capable of altering the sample collections in any significant manner. Repeat sampling will allow us to understand how routine use of these labs affects the microbial ecology over time.
    Keywords: Space Sciences (General)
    Type: JSC-E-DAA-TN52831 , COSPAR Scientific Assembly; Jul 14, 2018 - Jul 22, 2018; Pasadena, CA; United States
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  • 10
    Publication Date: 2019-07-13
    Description: The Habitable Exoplanet Observatory (HabEx) mission has unique optical performance requirements which drive the mirror design process beyond the traditional criteria. While mass and stiffness are still important, the response to inertia loading (expressed in terms of Zernike coefficients) to omni-directional excitation dominates the effort. While a Zerodur mirror is the current baseline, as mass budgets change, a ULE design is being studied as a potential alternative. This trade study looked at over 264 design variations using the Arnold Mirror Modeler and ANSYS(c) to investigate the influence of various design elements, including: substrate thickness, core cell size, hexapod geometry and local reinforcement. Design 'goodness' was evaluated based on the mirror's inertial deformation response to omni-directional input. This response was calculated via RSSing Zernike polynomial responses to (XYZ) accelerations.
    Keywords: Space Sciences (General)
    Type: MSFC-E-DAA-TN61193 , Optics and Photonics Conference Proceedings; Aug 19, 2018 - Aug 23, 2018; San Diego, CA; United States
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