SPP NEO Inactive Body Small Planetary Platforms Assessment for NEO Inactive Bodies

SPP NEO Inactive Body Small Planetary Platforms Assessment for NEO Inactive Bodies

CDF STUDY REPORT SPP NEO Inactive Body Small Planetary Platforms Assessment for NEO Inactive Bodies CDF-178(A) January 2018 SPP NEO Inactive Body CDF Study Report: CDF-178(A) January 2018 page 1 of 209 CDF Study Report SPP NEO Inactive Body Small Planetary Platforms Assessment for NEO Inactive Bodies ESA UNCLASSIFIED – Releasable to the Public SPP NEO Inactive Body CDF Study Report: CDF-178(A) January 2018 page 2 of 209 FRONT COVER Study Logo showing satellite approaching an asteroid with a swarm of SmallSats ESA UNCLASSIFIED – Releasable to the Public SPP NEO Inactive Body CDF Study Report: CDF-178(A) January 2018 page 3 of 209 STUDY TEAM This study was performed in the ESTEC Concurrent Design Facility (CDF) by the following interdisciplinary team: TEAM LEADER AOCS PAYLOAD COMMUNICATIONS POWER CONFIGURATION PROGRAMMATICS/ AIV COST ELECTRICAL PROPULSION DATA HANDLING CHEMICAL PROPULSION GS&OPS SYSTEMS MISSION ANALYSIS THERMAL MECHANISMS Under the responsibility of: S. Bayon, SCI-FMP, Study Manager With the scientific assistance of: Study Scientist With the technical support of: Systems/APIES Smallsats Radiation The editing and compilation of this report has been provided by: Technical Author ESA UNCLASSIFIED – Releasable to the Public SPP NEO Inactive Body CDF Study Report: CDF-178(A) January 2018 page 4 of 209 This study is based on the ESA CDF Open Concurrent Design Tool (OCDT), which is a community software tool released under ESA licence. All rights reserved. Further information and/or additional copies of the report can be requested from: S. Bayon ESA/ESTEC/SCI-FMP Postbus 299 2200 AG Noordwijk The Netherlands Tel: +31-(0)71-5655502 Fax: +31-(0)71-5655985 [email protected] For further information on the Concurrent Design Facility please contact: M. Bandecchi ESA/ESTEC/TEC-SYE Postbus 299 2200 AG Noordwijk The Netherlands Tel: +31-(0)71-5653701 Fax: +31-(0)71-5656024 [email protected] ESA UNCLASSIFIED – Releasable to the Public SPP NEO Inactive Body CDF Study Report: CDF-178(A) January 2018 page 5 of 209 TABLE OF CONTENTS 1 INTRODUCTION .................................................................................. 13 1.1 Background ...........................................................................................................13 1.2 Objective ................................................................................................................13 1.3 Scope .....................................................................................................................13 1.4 Document Structure ............................................................................................. 14 2 PAYLOAD ............................................................................................ 15 2.1 Requirements and Design Drivers MC ................................................................. 15 2.2 Requirements and Design Drivers SS ................................................................... 15 2.3 Assumptions and Trade offs SS ........................................................................... 16 2.3.1 Assumptions ................................................................................................... 16 2.3.2 Trade Offs and Selection of Instruments ....................................................... 16 2.4 Baseline Design SS ............................................................................................... 19 2.5 Accommodation ................................................................................................... 19 2.6 Operational Aspects ............................................................................................. 20 2.7 Data Volume ......................................................................................................... 21 3 MISSION ANALYSIS ........................................................................... 23 3.1 Requirements and Design Drivers MC ................................................................ 23 3.1.1 Multipoint Mission ........................................................................................ 23 3.1.2 Launch Vehicle ............................................................................................... 23 3.1.3 Launch Date ................................................................................................... 23 3.1.4 Transfer Duration .......................................................................................... 23 3.1.5 Duration of Operations .................................................................................. 23 3.2 Assumptions and Trade-Offs MC ........................................................................ 24 3.2.1 Small Body Classification ............................................................................... 24 3.2.2 Launch Strategies and Trade-Offs ................................................................. 26 3.2.3 Preliminary Assessment of DIFFERENT MISSIONS ................................... 29 3.3 Baseline Design MC ..............................................................................................31 3.3.1 Target Selection...............................................................................................31 3.3.2 Apophis ...........................................................................................................31 3.3.3 Launch Scenario ............................................................................................. 35 3.3.4 Transfers to Apophis ...................................................................................... 37 3.4 Sensitivity Analysis for MC: What if? .................................................................. 44 3.4.1 Launch into LEO + EP Assisted Escape ........................................................ 44 3.4.2 Other NEOs Targets ....................................................................................... 45 3.4.3 Mission to Phobos .......................................................................................... 48 4 SYSTEMS ............................................................................................ 53 4.1 System Requirements and Design Drivers .......................................................... 53 4.1.1 Mission and System Requirements Tree ....................................................... 53 4.1.2 Mission Requirements Update ...................................................................... 53 4.1.3 Mission Design Drivers .................................................................................. 57 ESA UNCLASSIFIED – Releasable to the Public SPP NEO Inactive Body CDF Study Report: CDF-178(A) January 2018 page 6 of 209 4.2 System Baseline Design ....................................................................................... 58 4.2.1 Target Selection and Strawman Payload ....................................................... 58 4.2.2 Transfer, Rendezvous and Operations Overview .......................................... 59 4.2.3 Baseline MC Design Summary ....................................................................... 60 4.2.4 Baseline SS Design Summary ........................................................................ 62 4.2.5 Propellant Budget .......................................................................................... 62 4.2.6 Product Tree ................................................................................................... 63 4.2.7 Modes and Phases .......................................................................................... 65 4.2.8 Smallsat Mass Budget and Equipment List ................................................... 66 4.2.9 Mother Spacecraft Mass Budget and Equipment List ................................... 68 4.2.10 Power Budget ................................................................................................. 70 4.2.11 Structural Assumptions .................................................................................. 71 4.3 System Options ..................................................................................................... 71 5 CONFIGURATION ............................................................................... 73 5.1 Requirements and Design Drivers MC ................................................................ 73 5.2 Requirements and Design Drivers SS .................................................................. 73 5.3 Assumptions and Trade offs MC .......................................................................... 74 5.4 Assumptions and Trade offs SS ........................................................................... 74 5.5 Baseline Design MC ............................................................................................. 74 5.5.1 Description of the MC Spacecraft .................................................................. 74 5.5.2 Main Dimensions of the MC spacecraft ......................................................... 81 5.6 Baseline Design SS ............................................................................................... 82 5.6.1 Description of the SS Spacecraft .................................................................... 82 5.6.2 Main Dimensions of the SS Spacecraft .......................................................... 84 6 MECHANISMS ..................................................................................... 87 6.1 Requirements and Design Drivers MC ...............................................................

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