ESA Document - Emits - ESA
ESA Document - Emits - ESA ESA Document - Emits - ESA
s EVA Airlock 1 Back Node Service Platform 2 Habitation Module Figure 2-52: Launch of TEI and MOI 2.8.3.5 Launches 9-17- TMI stages 2 & 3 assembly Service Platform 3 Front Node HMM Assessment Study Report: CDF-20(A) February 2004 page 96 of 422 • Addition of TMI stage 2 & 3 Propulsion Stages – Launch 9- Central structure + SP4 – Each propulsion stack is captured & berthed by Robotic arm from service platform – Each propulsion stack will require a Launcher upper stage to provide rendezvous capability. Service Platform 4 EVA Airlock 1 Back Node Service Platform 2 Figure 2-53: Launch of 2 nd and 3 rd stage of TMI 2.8.3.6 Launches 18-22- TMI stage 1 assembly Habitation Module • Addition of TMI stage 1 Propulsion Stages – – Launch 18- Central structure + SP5 • Disposal of SP4 prior to berthing – Launch 19-22- Propulsion stacks – Each propulsion stack is captured & berthed by Robotic arm from service platform Service Platform 3 Front Node
s HMM Assessment Study Report: CDF-20(A) February 2004 page 97 of 422 – Each propulsion stack will require a Launcher upper stage to provide rendezvous capability. Service Platform 5 Figure 2-54: Launch of TMI stage 1 2.8.3.7 Launch 23- ERC and ‘appendage’ assembly • Addition of ERC and Appendages – ERC – Four Solar Arrays (EVA-assisted Assembly) – Two Antennas (EVA-assisted Assembly) • Disposal of SP2 prior to ERC docking EVA Airlock 1 Back Node Service Platform 2 – Launch Mass (Estimated) – ERC will require a launcher upper stage to provide rendezvous and docking capability. – Appendages will require disposable support structure (possible component of disposable upper stage) and will require EVA-assisted assembly by robotic arm from service platform. Service Platform 5 EVA Airlock 1 Figure 2-55: Launch of ERC and appendage 2.8.3.8 Launches 24-25- Composite completion • Resupply, Crew Transfer, Re-fuel & Addition of MEV prior to service platform disposal – Launch 24 - Consumables (Re) Supply – Service platform disposal to free port for MEV – Post service platform disposal • Launch 25 – MEV Habitation Module Habitation Module Service Platform 3 Front Node Service Platform 3
- Page 45 and 46: s Mars Excursion Vehicle Transfer H
- Page 47 and 48: s 2.7.5.1 Mission elements dry mass
- Page 49 and 50: s 2.7.5.8 MEV release The MEV is re
- Page 51 and 52: s Total mission time (days) 1200 10
- Page 53 and 54: s HMM Assessment Study Report: CDF-
- Page 55 and 56: s HMM Assessment Study Report: CDF-
- Page 57 and 58: s stack 9 Propellant mass of the ne
- Page 59 and 60: s HMM Assessment Study Report: CDF-
- Page 61 and 62: s HMM Assessment Study Report: CDF-
- Page 63 and 64: s HMM Assessment Study Report: CDF-
- Page 65 and 66: s The core supporting structure has
- Page 67 and 68: s 2.7.7.1.3 Mars excursion module S
- Page 69 and 70: s 2.7.7.1.4 Earth return capsule HM
- Page 71 and 72: s Mission Phase Description Event s
- Page 73 and 74: s Mission Phase Description Event s
- Page 75 and 76: s 2.7.10 Mission performance Table
- Page 77 and 78: s Days on Martian surface 450 400 3
- Page 79 and 80: s HMM Assessment Study Report: CDF-
- Page 81 and 82: s HMM Assessment Study Report: CDF-
- Page 83 and 84: s Maximum manoeuvre duration 6 mont
- Page 85 and 86: s % of loss from baseline 20 18 16
- Page 87 and 88: s 2.7.15 Sensitivity analysis HMM A
- Page 89 and 90: s 2.7.15.4 Influence of the mass of
- Page 91 and 92: s HMM Assessment Study Report: CDF-
- Page 93 and 94: s Parameters used: • No Shuttle
- Page 95: s 2.8.3.3 Launch 3- Front node Figu
- Page 99 and 100: s HMM Assessment Study Report: CDF-
- Page 101 and 102: s HMM Assessment Study Report: CDF-
- Page 103 and 104: s HMM Assessment Study Report: CDF-
- Page 105 and 106: s HMM Assessment Study Report: CDF-
- Page 107 and 108: s HMM Assessment Study Report: CDF-
- Page 109 and 110: s 2.10.1.4 Communications HMM Asses
- Page 111 and 112: s HMM Assessment Study Report: CDF-
- Page 113 and 114: s 2.10.2.2.2 LEO assembly HMM Asses
- Page 115 and 116: s HMM Assessment Study Report: CDF-
- Page 117 and 118: s Basic RF link Four 70-m Ka-band s
- Page 119 and 120: s HMM Assessment Study Report: CDF-
- Page 121 and 122: s HMM Assessment Study Report: CDF-
- Page 123 and 124: s HMM Assessment Study Report: CDF-
- Page 125 and 126: s 3 TRANSFER VEHICLE 3.1 Systems…
- Page 127 and 128: s Operational Requirements It shall
- Page 129 and 130: s Trans Mars Injection Module Mars
- Page 131 and 132: s Figure 3-2: Parallel configuratio
- Page 133 and 134: s Figure 3-6: Global dimensions com
- Page 135 and 136: s Front Node 3.2.3.1.3 EVA systems
- Page 137 and 138: s Trans Mars Injection (three stage
- Page 139 and 140: s Figure 3-16: Recommendations for
- Page 141 and 142: s Factors to be considered Impacts
- Page 143 and 144: s HMM Assessment Study Report: CDF-
- Page 145 and 146: s HMM Assessment Study Report: CDF-
s<br />
EVA<br />
Airlock 1<br />
Back<br />
Node<br />
Service Platform 2<br />
Habitation Module<br />
Figure 2-52: Launch of TEI and MOI<br />
2.8.3.5 Launches 9-17- TMI stages 2 & 3 assembly<br />
Service Platform 3<br />
Front<br />
Node<br />
HMM<br />
Assessment Study<br />
Report: CDF-20(A)<br />
February 2004<br />
page 96 of 422<br />
• Addition of TMI stage 2 & 3 Propulsion Stages<br />
– Launch 9- Central structure + SP4<br />
– Each propulsion stack is captured & berthed by Robotic arm from service<br />
platform<br />
– Each propulsion stack will require a Launcher upper stage to provide rendezvous<br />
capability.<br />
Service Platform 4<br />
EVA<br />
Airlock 1<br />
Back<br />
Node<br />
Service Platform 2<br />
Figure 2-53: Launch of 2 nd and 3 rd stage of TMI<br />
2.8.3.6 Launches 18-22- TMI stage 1 assembly<br />
Habitation Module<br />
• Addition of TMI stage 1 Propulsion Stages –<br />
– Launch 18- Central structure + SP5<br />
• Disposal of SP4 prior to berthing<br />
– Launch 19-22- Propulsion stacks<br />
– Each propulsion stack is captured & berthed by Robotic arm from service<br />
platform<br />
Service Platform 3<br />
Front<br />
Node
Change language