NASA







Technology Gallery

2017

Select Gallery View : Slideshow | Thumbnails | PDF

slide photo
Slide 1 of 22

PhysCOS and COR Strategic Technology Portfolio


For more information about these technologies visit our Technology Database.

slide photo
slide photo
Slide 2 of 22

Thin single-crystal silicon X-ray mirror segment (after trimming)


Significance: World-class thin grazing-angle X-ray mirror technology; baselined for Lynx X-ray flagship mission concept

Project Title: Next Generation X-ray Optics: High Resolution, Light Weight, and Low Cost

PI: Zhang, William (GSFC)

slide photo
slide photo
Slide 3 of 22

X-ray Critical-Angle Transmission (CAT) grating with quarter dollar coin for scale


Significance: Highest-resolution X-ray grating technology; baselined for Lynx X-ray flagship mission concept

Project Title: Development of a CAT Grating Spectrometer

PI: Mark Schattenburg (MIT Kavli Institute for Astrophysics and Space Research)

slide photo
slide photo
Slide 4 of 22

Modular BICEP3 Focal Plane for Cosmic Microwave Background (CMB) polarimetry


Significance: Developing antenna designs providing sensitivity, stability, and minimized particle susceptibility for bands required by the Inflation Probe, enabling identification of Inflation instants after the Big Bang

Project Title: Planar Antenna-Coupled Superconducting Detectors for CMB Polarimetry

PI: James Bock (JPL/Caltech)

slide photo
slide photo
Slide 5 of 22

Demonstration model array of Transition-Edge Sensors (TESs)


Significance: TES microcalorimeters offer energy resolution that may enable future missions such as the Lynx X-ray flagship mission concept

Project Title: Advanced X-ray Microcalorimeters: TES Microcalorimeters

PI: Caroline Kilbourne (GSFC)

slide photo
slide photo
Slide 6 of 22

Single-shell mounting concept with mounted adjustable X-ray mirror and electrical connections


Significance: Adjustable X-ray optics are a backup technology for the Lynx X-ray large mission concept

Project Title: Adjustable X-Ray Optic

PI: Paul Reid (SAO)

slide photo
slide photo
Slide 7 of 22

REXIS Detector Assembly Module (DAM) with directly deposited filter on the X-ray CCDs; REXIS is a student-built instrument deployed on the OSIRIS-REx mission to Asteroid Bennu


Significance: X-ray detectors operate far better when filters allow X-ray photons through and block longer wavelength light

Project Title: Directly-Deposited Blocking Filters for X-ray Imaging Detectors

PI: Mark Bautz (MIT Kavli Institute for Astrophysics and Space Research)

slide photo
slide photo
Slide 8 of 22

Digital Micro-mirror Device (DMD) undergoing vibration testing as part of flight qualification


Significance: Replacing windows of commercially available DMDs may enable far-UV multi-object spectrometry in future missi

Project Title: Development of DMDs for Far-UV Applications

PI: Zoran Ninkov (RIT)

slide photo
slide photo
Slide 9 of 22

Selected parts for 4-to-0.05-K for Continuous Adiabatic Demagnetization Refrigerator (CADR) cooling system fabricated at GSFC


Significance: This advanced sub-Kelvin cooling technology has been baselined by Lynx, Origins, PICO, and GEP

Project Title: High-Efficiency Continuous Cooling for Cryogenic Instruments and sub-Kelvin Detectors

PI: James Tuttle (GSFC)

slide photo
Slide 10 of 22

1.5-m Harris mirror with support structure


Significance: This technology may enable required ultra-stability (~10 pm) for HabEx and LUVOIR missions

Project Title: Predictive Thermal Control (PTC) Technology to enable Thermally Stable Telescopes

PI: H. Philip Stahl (MSFC)

slide photo
slide photo
Slide 11 of 22

First resonance measurements of mock Cosmic Microwave Background (CMB) detector array


Significance: This and related technologies may enable future CMB missions, e.g. LiteBIRD

Project Title: Technology Development for LiteBIRD and other CMB Missions

PI: Adrian T. Lee (UC Berkeley)

slide photo
slide photo
Slide 12 of 22

Atomic Layer Deposition (ALD) Multi-Channel Plate (MCP) image detail


Significance: This detector technology is baselined by HabEx, LUVOIR, and CETUS for UV/Visible light detection

Project Title: High-Performance Sealed-Tube Cross-Strip (XS) Photon-Counting Sensors for UV-Vis Astrophysics Instruments

PI: Oswald Siegmund (UC Berkeley)

slide photo
slide photo
Slide 13 of 22

Molecular Beam Epitaxy (MBE) system at JPL used for coating advanced detectors


Significance: Advanced detectors developed by this project are baselined by SHIELDS, HabEx, LUVOIR, and ground facilities are fabricated using Atomic Layer Deposition (ALD) coatings

Project Title: Advanced FUV/UV/Visible Photon-Counting and Ultralow-Noise Detectors

PI: Shouleh Nikzad (JPL/Caltech)

slide photo
slide photo
Slide 14 of 22

100×100 mm2 Multi-Channel Plate (MCP) detector mounted on vacuum test system


Significance: Large-format low-noise detectors may enable future far-UV missions

Project Title: Development of 100×100 mm2 photon-counting UV detectors

PI: John Vallerga (UC Berkeley)

slide photo
slide photo
Slide 15 of 22

Stratospheric Terahertz Observatory (STO2)Balloon-borne observatory being prepared for launch in Antarctica; an early working device was provided by this team to fly on STO2 in 2016


Significance: This technology provides 4.7-THz Local Oscillators (LOs), enabling far-IR/sub-mm missions such as the balloon-borne Galactic/Extragalactic ULDB Spectroscopic Terahertz Observatory (GUSTO)

Project Title: Raising the Technology Readiness of 4.7-THz local oscillators

PI: Qing Hu (MIT)

slide photo
slide photo
Slide 16 of 22

40-GHz and 90-GHz feedhorn-coupled focal plane arrays for performing Cosmic Microwave Background (CMB) measurements


Significance: : CMB measurements may enable identification of the “Inflation” cosmologists believe may have occurred instants after the Big Bang; multi-wavelength measurements can help remove foreground noise

Project Title: High Efficiency Feedhorn-Coupled TES-based Detectors for CMB Polarization

PI: Edward Wollack (GSFC)

slide photo
slide photo
Slide 17 of 22

Busek components developed for colloid microthrusters for precision spacecraft control


Significance: Microthrusters are critical for controlling the spacecraft of future missions such as the Laser Interferometer Space Antenna (LISA) gravitational-wave observatory

Project Title: LISA Colloid Microthruster Technology

PI: John Ziemer (JPL)

slide photo
slide photo
Slide 18 of 22

Prototype Laser Interferometer Space Antenna (LISA) telescope designed for room-temp testing


Significance: The LISA gravitational-wave observatory crucially depends on collecting laser light from a remote spacecraft, millions of km away

Project Title: Telescope Development for the LISA Mission

PI: Jeffrey Livas (GSFC)

slide photo
slide photo
Slide 19 of 22

Prototype laser power amplifier for lasers enabling the Laser Interferometer Space Antenna (LISA) gravitational-wave observatory


Significance: LISA crucially depends on lasers to allow interferometric measurement of the multi-million-km distance between the three spacecraft

Project Title: Laser Technology Development Project for the LISA Mission

PI: Anthony Yu (GSFC)

slide photo
slide photo
Slide 20 of 22

Torsion pendulum test-bed for gravitational reference sensors used for testing charge management system for the Laser Interferometer Space Antenna (LISA) gravitational-wave observatory


Significance: LISA crucially depends on charge management to prevent electrostatic noise interfering with interferometric measurement of the multi-million-km distance between the three spacecraft

Project Title: UV LED-based Charge Management System for LISA

PI: John Conklin (University of Florida)

slide photo
slide photo
Slide 21 of 22

Interferometer testbed built to demonstrate phasemeter and measurement system performance developed for the Laser Interferometer Space Antenna (LISA) gravitational-wave observatory


Significance: LISA needs a phasemeter system to allow interferometric measurement of the multi-million-km distance between the three spacecraft

Project Title: LISA Phasemeter Project

PI: William Klipstein (JPL)

slide photo
slide photo
Slide 22 of 22

Lab test setup for picometer measurement of mirror dynamics


Significance:Ultra-stability and -precision (~10 pm) may enable the HabEx and LUVOIR missions

Project Title: Ultra-Stable Structure

PI: Babak Saif (GSFC)

slide photo
PhysCOS and COR Strategic Technology Portfolio

PhysCOS and COR Strategic Technology Portfolio


For more information about these technologies visit our Technology Database.




slide image

Thin single-crystal silicon X-ray mirror segment (after trimming)


Significance: World-class thin grazing-angle X-ray mirror technology; baselined for Lynx X-ray flagship mission concept

Project Title: Next Generation X-ray Optics: High Resolution, Light Weight, and Low Cost

PI: Zhang, William (GSFC)




slide image

X-ray Critical-Angle Transmission (CAT) grating with quarter dollar coin for scale


Significance: Highest-resolution X-ray grating technology; baselined for Lynx X-ray flagship mission concept

Project Title: Development of a CAT Grating Spectrometer

PI: Mark Schattenburg (MIT Kavli Institute for Astrophysics and Space Research)




slide image

Modular BICEP3 Focal Plane for Cosmic Microwave Background (CMB) polarimetry


Significance: Developing antenna designs providing sensitivity, stability, and minimized particle susceptibility for bands required by the Inflation Probe, enabling identification of Inflation instants after the Big Bang

Project Title: Planar Antenna-Coupled Superconducting Detectors for CMB Polarimetry

PI: James Bock (JPL/Caltech)




slide image

Demonstration model array of Transition-Edge Sensors (TESs)


Significance: TES microcalorimeters offer energy resolution that may enable future missions such as the Lynx X-ray flagship mission concept

Project Title: Advanced X-ray Microcalorimeters: TES Microcalorimeters

PI: Caroline Kilbourne (GSFC)




slide image

Single-shell mounting concept with mounted adjustable X-ray mirror and electrical connections


Significance: Adjustable X-ray optics are a backup technology for the Lynx X-ray large mission concept

Project Title: Adjustable X-Ray Optic

PI: Paul Reid (SAO)




slide image

REXIS Detector Assembly Module (DAM) with directly deposited filter on the X-ray CCDs; REXIS is a student-built instrument deployed on the OSIRIS-REx mission to Asteroid Bennu


Significance: X-ray detectors operate far better when filters allow X-ray photons through and block longer wavelength light

Project Title: Directly-Deposited Blocking Filters for X-ray Imaging Detectors

PI: Mark Bautz (MIT Kavli Institute for Astrophysics and Space Research)




slide image

Digital Micro-mirror Device (DMD) undergoing vibration testing as part of flight qualification


Significance: Replacing windows of commercially available DMDs may enable far-UV multi-object spectrometry in future missi

Project Title: Development of DMDs for Far-UV Applications

PI: Zoran Ninkov (RIT)




slide image

Selected parts for 4-to-0.05-K for Continuous Adiabatic Demagnetization Refrigerator (CADR) cooling system fabricated at GSFC


Significance: This advanced sub-Kelvin cooling technology has been baselined by Lynx, Origins, PICO, and GEP

Project Title: High-Efficiency Continuous Cooling for Cryogenic Instruments and sub-Kelvin Detectors

PI: James Tuttle (GSFC)




slide image

1.5-m Harris mirror with support structure


Significance: This technology may enable required ultra-stability (~10 pm) for HabEx and LUVOIR missions

Project Title: Predictive Thermal Control (PTC) Technology to enable Thermally Stable Telescopes

PI: H. Philip Stahl (MSFC)




slide image

First resonance measurements of mock Cosmic Microwave Background (CMB) detector array


Significance: This and related technologies may enable future CMB missions, e.g. LiteBIRD

Project Title: Technology Development for LiteBIRD and other CMB Missions

PI: Adrian T. Lee (UC Berkeley)




slide image

Atomic Layer Deposition (ALD) Multi-Channel Plate (MCP) image detail


Significance: This detector technology is baselined by HabEx, LUVOIR, and CETUS for UV/Visible light detection

Project Title: High-Performance Sealed-Tube Cross-Strip (XS) Photon-Counting Sensors for UV-Vis Astrophysics Instruments

PI: Oswald Siegmund (UC Berkeley)




slide image

Molecular Beam Epitaxy (MBE) system at JPL used for coating advanced detectors


Significance: Advanced detectors developed by this project are baselined by SHIELDS, HabEx, LUVOIR, and ground facilities are fabricated using Atomic Layer Deposition (ALD) coatings

Project Title: Advanced FUV/UV/Visible Photon-Counting and Ultralow-Noise Detectors

PI: Shouleh Nikzad (JPL/Caltech)




slide image

100×100 mm2 Multi-Channel Plate (MCP) detector mounted on vacuum test system


Significance: Large-format low-noise detectors may enable future far-UV missions

Project Title: Development of 100×100 mm2 photon-counting UV detectors

PI: John Vallerga (UC Berkeley)




slide image

Stratospheric Terahertz Observatory (STO2) Balloon-borne observatory being prepared for launch in Antarctica; an early working device was provided by this team to fly on STO2 in 2016


Significance: This technology provides 4.7-THz Local Oscillators (LOs), enabling far-IR/sub-mm missions such as the balloon-borne Galactic/Extragalactic ULDB Spectroscopic Terahertz Observatory (GUSTO)

Project Title: Raising the Technology Readiness of 4.7-THz local oscillators

PI: Qing Hu (MIT)




slide image

40-GHz and 90-GHz feedhorn-coupled focal plane arrays for performing Cosmic Microwave Background (CMB) measurements


Significance: : CMB measurements may enable identification of the “Inflation” cosmologists believe may have occurred instants after the Big Bang; multi-wavelength measurements can help remove foreground noise

Project Title: High Efficiency Feedhorn-Coupled TES-based Detectors for CMB Polarization

PI: Edward Wollack (GSFC)




slide image

Busek components developed for colloid microthrusters for precision spacecraft control


Significance: Microthrusters are critical for controlling the spacecraft of future missions such as the Laser Interferometer Space Antenna (LISA) gravitational-wave observatory

Project Title: LISA Colloid Microthruster Technology

PI: John Ziemer (JPL)




slide image

Prototype Laser Interferometer Space Antenna (LISA) telescope designed for room-temp testing


Significance: The LISA gravitational-wave observatory crucially depends on collecting laser light from a remote spacecraft, millions of km away

Project Title: Telescope Development for the LISA Mission

PI: Jeffrey Livas (GSFC)




slide image

Prototype laser power amplifier for lasers enabling the Laser Interferometer Space Antenna (LISA) gravitational-wave observatory


Significance: LISA crucially depends on lasers to allow interferometric measurement of the multi-million-km distance between the three spacecraft

Project Title: Laser Technology Development Project for the LISA Mission

PI: Anthony Yu (GSFC)




slide image

Torsion pendulum test-bed for gravitational reference sensors used for testing charge management system for the Laser Interferometer Space Antenna (LISA) gravitational-wave observatory


Significance: LISA crucially depends on charge management to prevent electrostatic noise interfering with interferometric measurement of the multi-million-km distance between the three spacecraft

Project Title: UV LED-based Charge Management System for LISA

PI: John Conklin (University of Florida)




slide image

Interferometer testbed built to demonstrate phasemeter and measurement system performance developed for the Laser Interferometer Space Antenna (LISA) gravitational-wave observatory


Significance: LISA needs a phasemeter system to allow interferometric measurement of the multi-million-km distance between the three spacecraft

Project Title: LISA Phasemeter Project

PI: William Klipstein (JPL)




slide image

Lab test setup for picometer measurement of mirror dynamics


Significance:Ultra-stability and -precision (~10 pm) may enable the HabEx and LUVOIR missions

Project Title: Ultra-Stable Structure

PI: Babak Saif (GSFC)







View Gallery Collection by Year : '22 | '21 | '20 | '19 | '18 | '17 | '16 | '15 | '14 | '13 | '12







NASA logo Goddard Space Flight Center