ESA Document - Emits - ESA

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HMM
Assessment Study
Report: CDF-20(A)
February 2004
page 319 of 422
Element 2: Surface Habitation Module
MASS [kg]
DIMENSIONS [m]
Unit Element 2 Unit Name
Quantity Mass per Maturity Level Margin Total Mass Dim1 Dim2 Dim3
Click on button below to insert new unit
quantity
incl. margin Length Width Height
1 Antenna Pointing Mechanism 2 1.0 To be modified 10 2.2 0.15 0.15 0.15
2 Deployment Boom 2 2.0 To be modified 10 4.4
3 Hatch Door- Airlock 1 28.5 To be developed 20 34.2 0.9
4 Hatch Door Locking Mechanisms- Airlock 1 120.0 To be developed 20 144.0 0.95 0.8 0.05
5 Hatch Door- EVA Suit 4 34.20 To be developed 20 164.2
6 Hatch Door Locking Mechanisms- EVA Suit 4 144.0 To be developed 20 691.2
7 Sample Bio-Lock- Quarantine Chamber 10 22.4 To be developed 20 268.8 360.0 270.0
8 Clamp-band- SHM/MAV I/F 1 15.6 To be modified 10 17.2 1.2
9 APM Electronics 1 1.0 To be modified 10 1.1
10 Landing Leg Locking System 4 5.0 To be developed 20 24.0
- Click on button below to insert new unit
To be developed 20 0.0
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ELEMENT 2 SUBSYSTEM TOTAL
10 1128.0 19.8 1351.3
Table 4-25: Mass budget
Note that the masses stated for the EVA and egress hatch and locking mechanisms are bestestimate
figures.
Element 2: Surface Habitation Module
PPEAK AND POWER SPECIFICATION PER MODE
Unit Element 2 Unit Name Quantity Ppeak DESM DESM DESM SDAYM SDAYM SDAYM SNGM SNGM SNGM
Click on button below to insert new unit Pon Pstby Dc Pon Pstby Dc Pon Pstby Dc
1 Antenna Pointing Mechanism 2 10.0 100.0 10.0 100.0
2 Deployment Boom 2
3 Hatch Door- Airlock 1
4 Hatch Door Locking Mechanisms- Airlock 1
5 Hatch Door- EVA Suit 4
6 Hatch Door Locking Mechanisms- EVA Suit 4
7 Sample Bio-Lock- Quarantine Chamber 10
8 Clamp-band- SHM/MAV I/F 1
9 APM Electronics 1 5.0 100.0 5.0 100.0
10 Landing Leg Locking System 4
- Click on button below to insert new unit
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ELEMENT 2 SUBSYSTEM TOTAL
10 0.0 0.0 0.0 15.0 0.0 15.0 0.0
4.3.8.5 Options
Table 4-26: Power budget
Further study of the lock and sealed I/F of the externally mounted EVA suits is required. Suitable
decontamination methods need to be considered to guarantee no contamination can enter the
habitable volume.
4.3.9 Sample handling
4.3.9.1 Requirements and design drivers
The following requirements are imposed upon the samples and the sample handling systems
1 COSPAR Planetary Protection rules apply:
• Category V applicable- In summary the following text applies:
• Category V missions comprise all Earth-return missions. The concern for these
missions is the protection of the terrestrial system, the Earth and the Moon. For
Category V missions, in a subcategory defined as “restricted Earth return,” the
highest degree of concern is expressed by the absolute prohibition of destructive
impact upon return, the need for containment throughout the return phase of all
returned hardware which directly contacted the target body or un-sterilzed
material from the body, and the need for containment of any un-sterilised sample