ESA Document - Emits - ESA
ESA Document - Emits - ESA ESA Document - Emits - ESA
s – ATV LEO reboost capability • Two on-axis ports available – One for further assembly operations – One for on-orbit resupply on service platform (Soyuz or ATV typical) – Alternative port required if Shuttle used for crew transfer 2.8.3.2 Launch 2- Back node LEO AOCS + Power Module + Workbench + EVA Airlock Habitation Module TV LEO Bench Figure 2-49: THM central cylinder and SP1 • Addition of Back Node • Addition of mission Flight EVA Airlock • Addition of Service Platform 2 (SP2) – LEO AOCS – LEO Power – Berthing Arm • EVA Operations required to complete assembly EVA Airlock 1 Back Node Service Platform 2 Service Platform 1 Habitation Module TV Service Platform HMM Assessment Study Report: CDF-20(A) February 2004 page 94 of 422
s 2.8.3.3 Launch 3- Front node Figure 2-50: Launch of Back Node and SP2 • Addition of Front Node – With Cupola • Disposal or Relocation of SP1 • Addition of SP3 (if no relocation of SP1) – LEO AOCS – LEO Power – Rendezvous Booster- TBD – EVA Airlock capability – LEO Crew Habitation – ATV LEO re-boost capability • EVA Operations required to complete assembly EVA Airlock 1 Back Node Service Platform 2 2.8.3.4 Launches 4-8- TEI & MOI assembly Habitation Module Service Platform 3 Front Node Figure 2-51: Launch of Front Node HMM Assessment Study Report: CDF-20(A) February 2004 page 95 of 422 • Addition of TEI & MOI Propulsion stages – Assume TEI stage is the central structure or TEI within central back-bone structure – 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
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- 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
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- Page 77 and 78: s Days on Martian surface 450 400 3
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- Page 83 and 84: s Maximum manoeuvre duration 6 mont
- Page 85 and 86: s % of loss from baseline 20 18 16
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- Page 125 and 126: s 3 TRANSFER VEHICLE 3.1 Systems…
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s<br />
– ATV LEO reboost capability<br />
• Two on-axis ports available<br />
– One for further assembly operations<br />
– One for on-orbit resupply on service platform (Soyuz or ATV typical)<br />
– Alternative port required if Shuttle used for crew transfer<br />
2.8.3.2 Launch 2- Back node<br />
LEO AOCS +<br />
Power Module +<br />
Workbench +<br />
EVA Airlock<br />
Habitation Module<br />
TV<br />
LEO Bench<br />
Figure 2-49: THM central cylinder and SP1<br />
• Addition of Back Node<br />
• Addition of mission Flight EVA Airlock<br />
• Addition of Service Platform 2 (SP2)<br />
– LEO AOCS<br />
– LEO Power<br />
– Berthing Arm<br />
• EVA Operations required to complete assembly<br />
EVA<br />
Airlock 1<br />
Back<br />
Node<br />
Service Platform 2<br />
Service Platform 1<br />
Habitation Module<br />
TV<br />
Service Platform<br />
HMM<br />
Assessment Study<br />
Report: CDF-20(A)<br />
February 2004<br />
page 94 of 422
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