SBIR/STTR Research Award

Near-Zero CTE 3D Printed RoboSiC Deployable Truss Core Structures with Active Precision Adjustment

Award identifier 77487bcd0d6962b2b6b4e35fa10e3b54dffa085eca05ef09b890925b49913e02Awarding agency National Aeronautics and Space Administration

Award amount

$124,983

Program and phase

SBIR · Phase I

Award year

2018

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
GOODMAN TECHNOLOGIES LLC
Proposal award date
2018-07-27
Contract end date
2019-02-15
UEI
LLNARNNCWD35
Solicitation number
SBIR_18_P1
Topic code
S2

Research abstract

High-contrast (10-10) imaging and spectroscopy for exoplanet science is critically dependent on telescope optics and wavefront stability. A challenging requirement on the opto-mechanical system is that of wavefront error stability on the order of 10 pm RMS per wavefront control step (~10s of minutes). Goodman Technologies proposes a purposefully engineered 2nd Generation structural-grade “RoboSiC-S” to provide the degree of passive athermality required by the HaBEX, LUVOIR, eLISA, and LISA missions, concomitant with low areal density (4-5 kg/m2) and the ability to perform active precision adjustment. The combination of 3D/AM allows themanufacture of high structural efficiency pyramidal, tetrahedral or Kagome truss sandwich core configurations, honeycomb cores, or lattice cores. Clever core design provides the additional stability benefit of cryogenic damping. RoboSiC-S, at 298K, is predicted to have 12X and 2.5X better steady state stability, respectively, than Zerodur® and M55J/954-6 (using the composites cryo-CTE). The average value of the CTE for the JWST M55J/T300/954-6 composite over the 25-150K temperature range calculated from measured Backplane Stability Test Article strains is -0.3 ppm/K (V1 tubes) and -0.125 ppm/K (spanner tubes). For comparison, RoboSiC-S has predicted a CTE of <1 ppm/K from 20-180K, and near-0 CTE (0.027 ppm/K) from 20-60K. In addition to 3D/AM, electrical conductivity of RoboSiC-S allows precision threaded holes and bolts to employ a “bolt-together” approach such as was used for the composite mirror backplane of the JWST. Ultra-fine ¼-80 bolts with 0.25mm pitch threads can be used as positioning actuators for hinged components to provide stable, athermal, and precision alignment. We plan a well-designed project to demonstrate a deployable primary mirror with backing structure, hinges, latches with stability to picometers, areal density of 4-5 kg/m2, and packaging efficiency of 7 deployed/stowed diameter.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Research funding history

21 SBIR/STTR records share this UEI (2017–2024). Reported award amounts total $10,900,715. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration

Agency intelligence

National Aeronautics and Space Administration

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