Artemis

Team Role:

George: Assistant for Everything

Ethan: Lead Designer

Jeffrey: Art Designer & Researcher

Jonathan: Lead Researcher

Jeremy: Lead Programmer

 Stored energy: 12.8V 20Ah Lithium Iron Phosphate Portable Rechargeable Battery(precharged)

 Source of energy: photoelectric effect -> electricity (using titanium of the body to transmit energy, and Venus's heat), and solar panels

 Rate at which the stored energy can be used: 80%, the other 20% is for emergency

 Self-discharge rate: 

 Volume: 1m x 1m x 3.3m = 3.3m^3

 Mass: ~931kg

 Operation temperature range:

 Using the energy released on atmospheric entry and descent: No

 Use of active materials (e.g., in the case of a battery, the anode, cathode, separator, electrolyte materials): Yes

 Whether a protective enclosure is required: Yes

 Whether the system can be operated in any orientation: Yes?

 Whether the system uses in situ resources from Venus (e.g., CO2): Yes, heat

 Whether the system can be recharged: Yes

 Whether the system can tolerate the forces and vibrations due to launch, reentry, descent, and landing: Yes?

 Whether the system can tolerate partial failure and still provide energy: Yes

bibliography:

https://adsabs.harvard.edu/pdf/2004ESASP.544...37B

https://cdn.website-editor.net/b01e838e55984754bac4e20b4502f6c2/files/uploaded/Silfab-SIL-370-NX-TITAN.pdf