Details
Originalsprache | Englisch |
---|---|
Aufsatznummer | 195004 |
Fachzeitschrift | Classical and quantum gravity |
Jahrgang | 31 |
Ausgabenummer | 19 |
Publikationsstatus | Veröffentlicht - Okt. 2014 |
Abstract
We report on the successful testing of the GRACE follow-on triple mirror assembly (TMA) prototype. This component serves to route the laser beam in a proposed follow-on mission to the Gravity Recovery and Climate Explorer (GRACE) mission, containing an optical instrument for space-based distance measurement between satellites. As part of this, the TMA has to meet a set of stringent requirements on both the optical and mechanical properties. The purpose of the TMA prototype testing is to establish the feasibility of the design, materials choice and fabrication techniques. Here we report on co-alignment testing of this device to the arc second (5 μrad) level and thermal alignment stability testing to 1 μrad K-1.
ASJC Scopus Sachgebiete
- Physik und Astronomie (insg.)
- Physik und Astronomie (sonstige)
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in: Classical and quantum gravity, Jahrgang 31, Nr. 19, 195004, 10.2014.
Publikation: Beitrag in Fachzeitschrift › Artikel › Forschung › Peer-Review
}
TY - JOUR
T1 - Testing the GRACE follow-on triple mirror assembly
AU - Fleddermann, R.
AU - Ward, R. L.
AU - Elliot, M.
AU - Wuchenich, D. M.
AU - Gilles, F.
AU - Herding, M.
AU - Nicklaus, K.
AU - Brown, J.
AU - Burke, J.
AU - Dligatch, S.
AU - Farrant, D. I.
AU - Green, K. L.
AU - Seckold, J. A.
AU - Blundell, M.
AU - Brister, R.
AU - Smith, C.
AU - Sheard, B. S.
AU - Heinzel, G.
AU - Danzmann, K.
AU - Klipstein, B.
AU - McClelland, D. E.
AU - Shaddock, D. A.
PY - 2014/10
Y1 - 2014/10
N2 - We report on the successful testing of the GRACE follow-on triple mirror assembly (TMA) prototype. This component serves to route the laser beam in a proposed follow-on mission to the Gravity Recovery and Climate Explorer (GRACE) mission, containing an optical instrument for space-based distance measurement between satellites. As part of this, the TMA has to meet a set of stringent requirements on both the optical and mechanical properties. The purpose of the TMA prototype testing is to establish the feasibility of the design, materials choice and fabrication techniques. Here we report on co-alignment testing of this device to the arc second (5 μrad) level and thermal alignment stability testing to 1 μrad K-1.
AB - We report on the successful testing of the GRACE follow-on triple mirror assembly (TMA) prototype. This component serves to route the laser beam in a proposed follow-on mission to the Gravity Recovery and Climate Explorer (GRACE) mission, containing an optical instrument for space-based distance measurement between satellites. As part of this, the TMA has to meet a set of stringent requirements on both the optical and mechanical properties. The purpose of the TMA prototype testing is to establish the feasibility of the design, materials choice and fabrication techniques. Here we report on co-alignment testing of this device to the arc second (5 μrad) level and thermal alignment stability testing to 1 μrad K-1.
KW - coalignment measurements
KW - GRACE
KW - GRACE follow-on
KW - gravity recovery and climate explorer
KW - laser ranging instrument
KW - retroreflectors
KW - triple mirror assembly
UR - http://www.scopus.com/inward/record.url?scp=84898834615&partnerID=8YFLogxK
U2 - 10.1088/0264-9381/31/19/195004
DO - 10.1088/0264-9381/31/19/195004
M3 - Article
AN - SCOPUS:84898834615
VL - 31
JO - Classical and quantum gravity
JF - Classical and quantum gravity
SN - 0264-9381
IS - 19
M1 - 195004
ER -