HERA MISSION. ESA UNCLASSIFIED - For Official Use
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1 HERA MISSION ESA UNCLASSIFIED - For Official Use
2 HERA/AIM mission scenario! First ever investigation of deflection test! Detailed analysis of impact crater (before/after impact or after only depending on DART launch)! First deep-space CubeSat! First binary asteroid and smallest ever asteroid visited
3 Launch dates! Soyuz launch from Kourou TBC in 2022 timeframe -> international collaboration! Didymos still a good target as of 2Q 2017, later launch opportunities: Departure date: 2023/10/22 Earth swing-by: 2024/10/26 Arrival date: 2026/09/02 Delta-V: km/s Departure date: 2024/10/14 Earth swing-by: N/A Arrival date: 2026/7/13 Delta-V: km/s A launch date in 2022 exists with arrival in 2024 but short development time, will be studied
4 DIDYMOS target! Didymoon size representative of a potentially hazardous object (generating casualties independently from impact location on Earth)! Shape and size of primary well known, not secondary! Asteroid observed by ground telescopes and radars! Heliocentric orbit well known Parameter Diameter(of(Primary(D P Diameter(of(Secondary(D S Value 0.780(km +/4 10% 0.163(km +/ (km Bulk(density(of(the(primary(ρ P 2104(kg(m 43 +/4 30% Distance(between(the(centre(of( primary(and(secondary(a orb Total(mass(of(system Rotation(period(of(the(primary 1.18(km +0.04/40.02(km 5.278e11(kg +/40.54e11(kg (h +/ (h Minimum Earth-Didymos distances: Sept 2022 > 0.07 AU (1.04e+7 km) Dec 2024 > 0.56 AU (8.37e+7 km) Jun 2026 > 0.90 AU (1.34e+8 km)
5 Spacecraft mass budget Subsystem Nominal Margin Total [kg] [%] [kg] EPS % 38.4 OBDH % 29.0 TT&C % 23.8 AOCS/GNC % 12.8 CPS % 53.8 TCS % 13.8 Harness % 32.1 Structure % Platform9total % Payload % 19.0 Payload9total % 19.0 Spacecraft dry9mass % SystemHmargin 20% 64.9 Spacecraft dry9mass +9 Margin PropellantHmass Pressurant 1.0 Spacecraft launch mass Launcher9performance (w.o.9adapter) Launcher9Margin Dry mass growth potential of 40kg for additional payload -> potential for international collaboration
6 POTENTIAL PAYLOAD CONTRIBUTIONS NAVCAM (In storage) 11.6 kg W 1.4 kg 9 W µlidar 14.9 kg (6U) CubeSat 2 x 1U payloads among:! Hyperspectral imaging! Volatiles! Relative Radioscience! Seismometry! Minearology! Dust environment! Gravimetry Option: study accommodation and release of JAXA s Small Carry-on Impactor Opportunities for additional international collaborations Additional Europeans interests expressed to ESA (to be discussed with MS in frame of B1): Radiation Monitor Micro-imagers Monostatic radar Thermal imager Multi-/hyper-spectral camera Bifocal metrology
7 HERA phase B1 (SSA + GSTP) Procurement proposals approved in IPC and Feb PB-SSA enabling CM19 preparation: HERA system Phase B1 study (co-funding GSTP 6 + SSA-NEO) K Technology developments and support activities: ISL breadboard (GSTP, G61M-005ET, PT) 250 K Engineering Model of a laser altimeter (GSTP, G61M-002EC, PT+PL+IE) 400 K HERA deep-space cubesat phase-a (GSTP) 400 K Asteroid environment analyses, simulations and science support (GSP) 500 K
8 HERA schedule Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 B1 B2-system B2 CD E1 PB-SSA / IPC DART PDR SRR CM19 PDR CDE1 conditional TEB START END PHASE Mar-18 Dec-18 Phase B1 ITT to be released latest in January 2018 Jan-19 Feb-19 SRR Feb-19 Dec-19 Phase B2-system Dec-19 CM19 *Sep-Nov 19: PhB2CD Conditional TEB Jan-20 May-20 Phase B2 May-20 Jul-20 PDR Aug-20 Aug-23 Phase CD Aug-23 Oct-23 Margin/Launch Campaign Oct-23 Launch
9 HERA Implementation! (Optional) programmatic frame to be agreed with MS before CM19: Space Safety! Participating States contribute to common costs pro-rata of their contribution.! In-kind contributions possible: e.g. technology, payload, facilities! Participation to the phase B1 important to consolidate system requirements for selected technologies through analyses and preliminary validation of algorithms! Preliminary CubeSat operations interfaces to be analysed and OIRD defined during phase B1! Phase B2 proposal (FFP) at the end of B1 and committed ceiling price financial proposal for C/D/E1 to be converted in FFP after CM19.
10 Conclusions! HERA provides a robust and cost effective means to perform a planetary defense validation test with a solid balance between risk and innovation.! HERA brings European industry one step forward in CubeSat relayed operations for future missions architectures (swarms in LEO, deep-space exploration).! Asteroid close-proximity operations provide optimal environement to test GNC solutions applicable to active debris removal and in-orbit servicing.! HERA provides unique visibility and public engagement in space activities! HERA maintains strong international collaboration with a robust schedule and clear interfaces.! Support from SMPAG is important to explain necessity for planeteray defense precursor mission
11 INSPIRATION AND OUTREACH sand art performance Asteroid Day press conf planetarii Astrofest (London, June 2016) Science&Vie Magazine PD videogame Design your asteroid Men vs Asteroid Discovery AD (Milan, 2016) Asteroid Day (Bucharest, 2015) school contest Channel documentary Science school book (Spain) CNN TV news Stephen Hawking supporting AD
12 HERA MISSION Ian Carnelli esa.int) Advanced Concepts and Studies office (TEC-SF)
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