LISA - Status at ESA. Oliver Jennrich LISA Project Scientist, ESA
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1 - Status at ESA Oliver Jennrich Project Scientist, ESA 1st -DECIGO Workshop, Sagamihara, / November 28
2 May 19: Proposed as a mission to the M3 project of Horizon 20. 1st -DECIGO Workshop, Sagamihara, / November 28 2
3 May 19: Proposed as a mission to the M3 project of Horizon spacecraft two-arm interometer heliocentric orbit Cigar-shaped spacecraft Cost: ~7 MAU, outside scope of an M-class mission 1st -DECIGO Workshop, Sagamihara, / November 28 3
4 May 19: Sagittarius 1st -DECIGO Workshop, Sagamihara, / November 28 4
5 May 19: Sagittarius 6 spacecraft, three-arm interometer Earth-orbit 1 million km baseline dust-bin shaped spacecraft Cost: ~7 MAU, outside scope of an M-class mission 1st -DECIGO Workshop, Sagamihara, / November 28 5
6 Dec 19: (G) proposed as cornerstone to Horizon 20+ 1st -DECIGO Workshop, Sagamihara, / November 28 6
7 Dec 19: (G) proposed as cornerstone to Horizon spacecraft, three-arm interferometer heliocentric orbit 5 million km baseline Cost: ~7 MAU 1st -DECIGO Workshop, Sagamihara, / November 28 7
8 19/19: cost reduction 1st -DECIGO Workshop, Sagamihara, / November 28 8
9 19/19: cost reduction Proposed NASA collaboration 3 spacecraft, three-arm interferometer smaller telescopes, drag free part of payload heliocentric orbit, 5 million km baseline Cost: 3-4 MAU 1st -DECIGO Workshop, Sagamihara, / November 28 9
10 19: ELITE proposal 1st -DECIGO Workshop, Sagamihara, / November 28
11 19: ELITE proposal First proposed as ELITE (European LIsa TEchnology ) in 19 Differential acceleration goal of -ms-2/ Hz over 1 1mHz Single payload Two inertial sensors, homodyne Michelson interferometer readout Geostationary orbit Target launch date of 22 1st -DECIGO Workshop, Sagamihara, / November 28
12 19-20: First industrial study Architecture essentially confirmed 3 S/C!"#$ 5 million km arm length 560,7&8*3)3,7&9*2'." heliocentric orbit, trailing Earth by 20 degree!"#$%&'(&")*&+,-*.&/0"*.(*.'1*"*.&!2,3*&40"*, Mass ~ kg Mission duration: 2 years, with consumables for years :'.*.&!,"*776"*0-%-"*1*&;1<=&&>&?,".,&?,.3'&!2,3*&>&47*,&4*.'-2,@6' 4#-".6,0& 9*-*,.3)& A*0".*&!*6<*.-$'.(& & >& & A*0".'-2,@6'& /",7%& & >& +4BCD&!E2E4E& & >& & +,-*.& F*0".#1 =,'G*.&&>&?,H>I7,J&/0-"6"#"&(K.&L#,0"*0'2"6J&&>&&MDC&5.,*&&>&&NG*.-6"%&'(&B6.0O),1 NG*.-6"%&'(&;7,-O'P&&>&&NG*.-6"%&'(&8.*0"' C!8CA&A'0".,3"&0'E&QRSRQTUUTD+T?! 9*2'."&D'E&+/>9I>:!>VVU 1st -DECIGO Workshop, Sagamihara, / November &WVVV
13 !"#$!"#$%&'(&")*&+,-*.&/0"*.(*.'1*"*.&!2,3*&40"*, 560,7&8*3)3,7&9*2'." 4#-".6,0& 9*-*,.3)& A*0".*&!*6<*.-$'.(& & >& & /",7%& & >& +4BCD&!E2E4E& & >& & +,-*.& F*0".#1 =,'G*.&&>&?,H>I7,J&/0-"6"#"&(K.&L#,0"*0'2"6J&&>&&MDC&5.,*&&>&&NG*.-6"%&'(&B6.0O),1 NG*.-6"%&'(&;7,-O'P&&>&&NG*.-6"%&'(&8.*0"' C!8CA&A'0".,3"&0'E&QRSRQTUUTD+T?! 9*2'."&D'E&+/>9I>:!>VVU 42.67&WVVV Nov 20: SMART2 study Two free-flying satellites with laser and microwave link Goal to demonstrate drag-free for and formation flying for Darwin Three payloads Technology Package US Technology Package Darwin Technology Package Approved by SPC in November 20 Launch window in 26 1st -DECIGO Workshop, Sagamihara, / November 28
14 !"#$!"#$%&'(&")*&+,-*.&/0"*.(*.'1*"*.&!2,3*&40"*, 560,7&8*3)3,7&9*2'." 4#-".6,0& 9*-*,.3)& A*0".*&!*6<*.-$'.(& & >& & /",7%& & >& +4BCD&!E2E4E& & >& & +,-*.& F*0".#1 =,'G*.&&>&?,H>I7,J&/0-"6"#"&(K.&L#,0"*0'2"6J&&>&&MDC&5.,*&&>&&NG*.-6"%&'(&B6.0O),1 NG*.-6"%&'(&;7,-O'P&&>&&NG*.-6"%&'(&8.*0"' C!8CA&A'0".,3"&0'E&QRSRQTUUTD+T?! 9*2'."&D'E&+/>9I>:!>VVU 42.67&WVVV July 24: LPF implementation Single spacecraft with two payloads European provided LTP NASA provided DRS Both payloads comprised: Two inertial sensors Laser metrology Micro-Newton Thrusters Laser metrology DFACS Lissajous orbit around L1 1st -DECIGO Workshop, Sagamihara, / November 28
15 !"#$!"#$%&'(&")*&+,-*.&/0"*.(*.'1*"*.&!2,3*&40"*, 560,7&8*3)3,7&9*2'." 4#-".6,0& 9*-*,.3)& A*0".*&!*6<*.-$'.(& & >& & /",7%& & >& +4BCD&!E2E4E& & >& & +,-*.& F*0".#1 =,'G*.&&>&?,H>I7,J&/0-"6"#"&(K.&L#,0"*0'2"6J&&>&&MDC&5.,*&&>&&NG*.-6"%&'(&B6.0O),1 NG*.-6"%&'(&;7,-O'P&&>&&NG*.-6"%&'(&8.*0"' C!8CA&A'0".,3"&0'E&QRSRQTUUTD+T?! 9*2'."&D'E&+/>9I>:!>VVU 42.67&WVVV July 25: Formulation starts Joint activity with NASA Industrial contract with EADS Astrium 1st -DECIGO Workshop, Sagamihara, / November 28
16 !"#$!"#$%&'(&")*&+,-*.&/0"*.(*.'1*"*.&!2,3*&40"*, 560,7&8*3)3,7&9*2'." 4#-".6,0& 9*-*,.3)& A*0".*&!*6<*.-$'.(& & >& & /",7%& & >& +4BCD&!E2E4E& & >& & +,-*.& F*0".#1 =,'G*.&&>&?,H>I7,J&/0-"6"#"&(K.&L#,0"*0'2"6J&&>&&MDC&5.,*&&>&&NG*.-6"%&'(&B6.0O),1 NG*.-6"%&'(&;7,-O'P&&>&&NG*.-6"%&'(&8.*0"' C!8CA&A'0".,3"&0'E&QRSRQTUUTD+T?! 9*2'."&D'E&+/>9I>:!>VVU 42.67&WVVV August 28: original end of formulation Joint activity with NASA Industrial contract with EADS Astrium Output: Baseline architecture Requirements and specifications Payload and system level Identification of technology development Mass ~ 55 kg 1st -DECIGO Workshop, Sagamihara, / November 28
17 !"#$!"#$%&'(&")*&+,-*.&/0"*.(*.'1*"*.&!2,3*&40"*, 560,7&8*3)3,7&9*2'." 4#-".6,0& 9*-*,.3)& A*0".*&!*6<*.-$'.(& & >& & /",7%& & >& +4BCD&!E2E4E& & >& & +,-*.& F*0".#1 =,'G*.&&>&?,H>I7,J&/0-"6"#"&(K.&L#,0"*0'2"6J&&>&&MDC&5.,*&&>&&NG*.-6"%&'(&B6.0O),1 NG*.-6"%&'(&;7,-O'P&&>&&NG*.-6"%&'(&8.*0"' C!8CA&A'0".,3"&0'E&QRSRQTUUTD+T?! 9*2'."&D'E&+/>9I>:!>VVU 42.67&WVVV June 28: updated technology plan Title Duration (months) Optical Assembly (OA) Articulation Mechanism Adjustable Frequency Reference for Laser Stabilisation 24 Opto-mechanical stability characterisation for 24 Metrology system for High-power laser system for 24 micropropulsion lifetime characterisation 36 GRS Front End Electronics characterisation for 24 Charge Management System for 24 Outgassing and Contamination characterisation for 24 Compact low noise magnetic gradiometer 1st -DECIGO Workshop, Sagamihara, / November 28
18 !"#$!"#$%&'(&")*&+,-*.&/0"*.(*.'1*"*.&!2,3*&40"*, 560,7&8*3)3,7&9*2'." 4#-".6,0& 9*-*,.3)& A*0".*&!*6<*.-$'.(& & >& & /",7%& & >& +4BCD&!E2E4E& & >& & +,-*.& F*0".#1 =,'G*.&&>&?,H>I7,J&/0-"6"#"&(K.&L#,0"*0'2"6J&&>&&MDC&5.,*&&>&&NG*.-6"%&'(&B6.0O),1 NG*.-6"%&'(&;7,-O'P&&>&&NG*.-6"%&'(&8.*0"' C!8CA&A'0".,3"&0'E&QRSRQTUUTD+T?! 9*2'."&D'E&+/>9I>:!>VVU 42.67&WVVV End 29: extended formulation Joint activity with NASA Industrial contract with EADS Astrium Baseline architecture Requirements and specifications Payload and system level Identification of technology development Mass ~ 55 kg Formulation extended to end 29 1st -DECIGO Workshop, Sagamihara, / November 28
19 !"#$!"#$%&'(&")*&+,-*.&/0"*.(*.'1*"*.&!2,3*&40"*, 560,7&8*3)3,7&9*2'." 4#-".6,0& 9*-*,.3)& A*0".*&!*6<*.-$'.(& & >& & /",7%& & >& +4BCD&!E2E4E& & >& & +,-*.& F*0".#1 =,'G*.&&>&?,H>I7,J&/0-"6"#"&(K.&L#,0"*0'2"6J&&>&&MDC&5.,*&&>&&NG*.-6"%&'(&B6.0O),1 NG*.-6"%&'(&;7,-O'P&&>&&NG*.-6"%&'(&8.*0"' C!8CA&A'0".,3"&0'E&QRSRQTUUTD+T?! 9*2'."&D'E&+/>9I>:!>VVU 42.67&WVVV End 29: Cosmic Vision Downselect I Cosmic Vision Long term science programme M missions ~3 M L missions 650 M, first launch (L1) ~28 Three missions identified for downselection in 29 as L1 candidate is L1 candidate 1st -DECIGO Workshop, Sagamihara, / November 28 19
20 !"#$!"#$%&'(&")*&+,-*.&/0"*.(*.'1*"*.&!2,3*&40"*, 560,7&8*3)3,7&9*2'." 4#-".6,0& 9*-*,.3)& A*0".*&!*6<*.-$'.(& & >& & /",7%& & >& +4BCD&!E2E4E& & >& & +,-*.& F*0".#1 =,'G*.&&>&?,H>I7,J&/0-"6"#"&(K.&L#,0"*0'2"6J&&>&&MDC&5.,*&&>&&NG*.-6"%&'(&B6.0O),1 NG*.-6"%&'(&;7,-O'P&&>&&NG*.-6"%&'(&8.*0"' C!8CA&A'0".,3"&0'E&QRSRQTUUTD+T?! 9*2'."&D'E&+/>9I>:!>VVU 42.67&WVVV 21: Cosmic Vision Downselect II Cosmic Vision Long term science programme M missions ~3 M L missions 650 M, first launch (L1) ~28 Three missions identified for downselection in 29 as L1 candidate is L1 candidate Selection for L1 in 21 1st -DECIGO Workshop, Sagamihara, / November 28 20
21 !"#$!"#$%&'(&")*&+,-*.&/0"*.(*.'1*"*.&!2,3*&40"*, 560,7&8*3)3,7&9*2'." 4#-".6,0& 9*-*,.3)& A*0".*&!*6<*.-$'.(& & >& & /",7%& & >& +4BCD&!E2E4E& & >& & +,-*.& F*0".#1 =,'G*.&&>&?,H>I7,J&/0-"6"#"&(K.&L#,0"*0'2"6J&&>&&MDC&5.,*&&>&&NG*.-6"%&'(&B6.0O),1 NG*.-6"%&'(&;7,-O'P&&>&&NG*.-6"%&'(&8.*0"' C!8CA&A'0".,3"&0'E&QRSRQTUUTD+T?! 9*2'."&D'E&+/>9I>:!>VVU 42.67&WVVV 21: Cosmic Vision Downselect II Cosmic Vision End 20: LPF launch! Long term science programme M missions ~3 M L missions 650 M, first launch (L1) ~28 Three missions identified for downselection in 29 as L1 candidate is L1 candidate Selection for L1 in 21 LPF launch end 20 1st -DECIGO Workshop, Sagamihara, / November 28 21
22 !"#$!"#$%&'(&")*&+,-*.&/0"*.(*.'1*"*.&!2,3*&40"*, 560,7&8*3)3,7&9*2'." 4#-".6,0& 9*-*,.3)& A*0".*&!*6<*.-$'.(& & >& & /",7%& & >& +4BCD&!E2E4E& & >& & +,-*.& F*0".#1 =,'G*.&&>&?,H>I7,J&/0-"6"#"&(K.&L#,0"*0'2"6J&&>&&MDC&5.,*&&>&&NG*.-6"%&'(&B6.0O),1 NG*.-6"%&'(&;7,-O'P&&>&&NG*.-6"%&'(&8.*0"' C!8CA&A'0".,3"&0'E&QRSRQTUUTD+T?! 9*2'."&D'E&+/>9I>:!>VVU 42.67&WVVV 22: Implementation phase If selected for L1 Move into implementation in 22 1st -DECIGO Workshop, Sagamihara, / November 28 22
23 !"#$!"#$%&'(&")*&+,-*.&/0"*.(*.'1*"*.&!2,3*&40"*, 560,7&8*3)3,7&9*2'." 4#-".6,0& 9*-*,.3)& A*0".*&!*6<*.-$'.(& & >& & /",7%& & >& +4BCD&!E2E4E& & >& & +,-*.& F*0".#1 =,'G*.&&>&?,H>I7,J&/0-"6"#"&(K.&L#,0"*0'2"6J&&>&&MDC&5.,*&&>&&NG*.-6"%&'(&B6.0O),1 NG*.-6"%&'(&;7,-O'P&&>&&NG*.-6"%&'(&8.*0"' C!8CA&A'0".,3"&0'E&QRSRQTUUTD+T?! 9*2'."&D'E&+/>9I>:!>VVU 42.67&WVVV 28: launch If selected for L1 Move into implementation in 22 Launch in 28 By 20, we will look at... 1st -DECIGO Workshop, Sagamihara, / November 28 23
24 The Gravitational Wave Sky 1st -DECIGO Workshop, Sagamihara, / November 28 24
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