Extra Eye Microdrone/meta
TL-12 Extra eye S variant
A small, lightweight, cheap, disposable sensor drone used for system surveys. A small folding solar cell array provides normal power for operation supplemented by a 1 MWs powercell.
Sensor is a combination of radio and broad spectrum electromagnetic scanner, giving sensor coverage from long wavelength radio to the far ultraviolet. This gives a good initial system survey, and the ability to note any anomalies which require more detailed analysis.
The low thrust (0.005 G) covers 1AU (150m km) in a little over 40 days, and 10 AU in 128 days.
Crew: 0 total. 0 crew stations covering vehicle maneuvering system, communicator, sensor. Subassemblies: Vehicle -4, Body -4. P&P: 1-MWs rechargeable power cell, 0.074 m^2 solar cell [Vehicle], 0.02 lbs. thrust standard thruster (no access space). Fuel: Occ: Cargo: Armor F RL B T U Body 4/40 4/40 4/40 4/40 4/40 Equipment Body: computer navigation program (C2); routine vehicle operation program (piloting-14, C4); sensor analysis (M/A) [4]-14; transmission profiling program (C3); PESA (scan 14, 3-mile range); medium range radio communicator (5,000-mile range); tiny computer (complexity 5; compact). Statistics Size: [LxWxH] 0.32 m x0.057 m x0.057 m Payload: 0 kg Lwt.: 1.67 kg Volume: 1.04 liter Maint.: 142 hours (0.676 mh/day) Price: Cr19,835 HT: 12 HP: 1 [Body]. Space Performance: sAccel (unloaded) 0.005 G, ( 0.005 G), sDecel 0.005 G, sMR 0.005, sAccel 0.161 kph/s. Design Notes: TL12 light frame cheap materials [Vehicle]. TL12 DR 40 advanced metal [Vehicle]. Operating Duration: 1 D 1 H 15 M 9 S. Vehicle Features: computerized controls, no streamlining. Volume: 1.04 liter [Body]. Area: 0.093 m^2 [Body]. Space Performance: Payload 0;
TL12 Extra eye R variant
A small, lightweight, cheap, disposable sensor drone used for system surveys. A small, short duration, unshielded RTG powers the on board equipment.
Sensor is a combination of radio and broad spectrum electromagnetic scanner, giving sensor coverage from long wavelength radio to the far ultraviolet. This gives a good initial system survey, and the ability to note any anomalies which require more detailed analysis.
The low thrust (0.022 G) covers 1AU (150m km) in a little over 19 days, and 10 AU in 61 days.
Crew: 0 total. 0 crew stations covering vehicle maneuvering system, communicator, sensor. Subassemblies: Vehicle -4, Body -4. P&P: 0.014-kW RTG (14 year duration; no access space), 0.08 lbs. thrust standard thruster (no access space). Fuel: Occ: Cargo: Armor F RL B T U Body 4/40 4/40 4/40 4/40 4/40 Equipment Body: computer navigation program (C2); routine vehicle operation program (piloting-14, C4); sensor analysis (M/A) [4]-14; transmission profiling program (C3); PESA (scan 14, 3-mile range); medium range radio communicator (5,000-mile range); tiny computer (complexity 5; compact). Statistics Size: [LxWxH] 0.32 m x0.057 m x0.057 m Payload: 0 kg Lwt.: 1.66 kg Volume: 1.05 liter Maint.: 135 hours (0.709 mh/day) Price: Cr21,808 HT: 12 HP: 1 [Body]. Space Performance: sAccel (unloaded) 0.022 G, ( 0.022 G), sDecel 0.022 G, sMR 0.022, sAccel 0.644 kph/s. Design Notes: TL12 light frame cheap materials [Vehicle]. TL12 DR 40 advanced metal [Vehicle]. Vehicle Features: computerized controls, no streamlining. Volume: 1.05 liter [Body]. Area: 0.093 m^2 [Body]. Space Performance: Payload 0;