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Statistics

Power and energy

A 50 kg URC rover draws about 249 W on average and can pull 3.7 kW for a few seconds, a ratio of roughly 15 to 1. The average is what sizes the battery; the peak is what sizes the fuse, the contactor and the parallel count of the pack. Between those two numbers sits the energy budget, and it is dominated by the one mission that may run for a full hour: the 60-minute Delivery requires 145 Wh of mission energy and 273 Wh of nameplate capacity at 50 kg. The sample is a parameter model of eight mission cases plus the eight packs teams have published.

249 WAverage draw50 kg rover, mixed mission loads2027 model
3.7 kWPeak drawAbout 15 times the average2027 model
273 WhNameplate for a 60-minute Delivery50 kg rover after margin and derating2027S-URC27-RULES
400–500 WhRecommended pack2.4–2.9 kg including BMS and enclosure2027

Key takeaways

  • Average and peak are separate budgets. The average sizes the cells; the peak sizes the protection. A 4P pack of 21700 cells is rated 180 A continuous, which is the minimum parallel count for a credible 156 A simultaneous peak, and that pack lands at about 496 Wh.
  • The 60-minute Delivery is the energy driver. Every other mission fits inside 106 Wh at 50 kg. Delivery is 37 % above the next largest and its clock is the longest in the rules, at up to 60 minutes.
  • Derating, not the cells, sets the nameplate. 145 Wh of mission energy becomes 273 Wh of nameplate through a 25 % margin and a combined usable fraction of 0.662.
  • Observed packs are 1.6 to 3.1 times the model. The six packs in the static figure hold 432 to 840 Wh, because current capacity, two missions on one charge and unmodelled hotel growth all push capacity up.

Average draw and peak draw

The subsystem power study produced a 50 kg, 35-minute load table at 249 W mean and 146 Wh, with a 3.7 kW everything-at-once peak. The mass-parameterised model reaches the same driving power from the other direction and splits it into mission stages, using the mission clocks published in the rules S-URC27-RULES §1.

Load 35 kg design 50 kg design Basis
Hotel load at the battery 46 W 63 W Compute, radios, cameras, fans, status lights and conversion loss
Drive, while driving 86 W 123 W 2.46 W/kg, rolling resistance 0.12, 3° mean grade, 0.8 m/s, efficiency 0.55
Arm, while active 20 W 29 W 3.0 W/kg of arm; arm is 19 % of rover mass
Science, while active 25 W 25 W Pumps, lamp, detector and heater; mass-independent
Credible simultaneous peak 156 A at 25.6 V, about 4.0 kW Climb, one stalled arm joint and hotel load

The hotel load is nearly mass-independent, rising 37 % for a 43 % increase in mass, while the drive load is proportional to mass. A light rover is hotel-dominated and a heavy rover is drive-dominated. The two peak estimates differ because they answer different questions: 3.7 kW is what happens if everything runs at once, and 4.0 kW is a credible simultaneous event. Either way the peak is 120 to 160 A at 24 to 26 V, against an average of 95 to 160 W.

Energy by mission

Rover Mission Minutes Mean power Energy
35 kg Astrobiology 30 93 W 46 Wh
35 kg Delivery 60 104 W 104 Wh
35 kg Equipment Servicing 30 69 W 35 Wh
35 kg Autonomy 40 114 W 76 Wh
50 kg Astrobiology 30 125 W 62 Wh
50 kg Delivery 60 145 W 145 Wh
50 kg Equipment Servicing 30 95 W 47 Wh
50 kg Autonomy 40 159 W 106 Wh
50 kg Autonomy then Servicing, one pack 70 153 Wh

These are model outputs, not measurements. The mission mixes that produce them are drive, arm, science and idle fractions estimated from the task content of each mission S-URC27-RULES §1.

Energy drawn against mission time, with the observed packs below
The upper panel is the model: energy against minutes on course at 35 kg and 50 kg, with the four mission windows marked and the 273 Wh nameplate requirement for the 50 kg, 60-minute case. The lower panel is the six packs teams actually field, from 432 to 840 Wh. The gap between the two is 1.6 to 3.1 times. Sample: model cases plus six published packs.Robotics Club @ Mississippi State University, 2026. Original analysis. S-URC27-RULES S-UIU-ROVER-PAGES-EARLIER-GE-02 Full resolution

From mission energy to a pack

Step 50 kg, one 60-minute Delivery Basis
Mission energy 145 Wh Model
Add 25 % mission margin 181 Wh Unmodelled hills, radio at maximum, extra arm moves
Divide by 0.80 depth of discharge 227 Wh 80 % discharge is about 400 cycles against 600 at 60 %
Divide by 0.92 for temperature and ageing 246 Wh 38 °C ambient plus end-of-life capacity loss
Divide by 0.90 path efficiency 273 Wh Sizing at the bus, not the cells
Combined usable fraction 0.662 0.80 × 0.92 × 0.90

The same chain gives 289 Wh for the back-to-back Autonomy then Equipment Servicing pair in one pack. The recommended pack for a first 2027 team is 400–500 Wh at 8S, lithium-ion 21700, 2.4–2.9 kg including BMS and enclosure. That covers the 289 Wh case with 38 to 73 % headroom, allows a second mission on one charge and keeps the pack small enough that a 4P current rating is comfortable.

Nameplate energy against pack mass for three chemistries
Pack-level energy against total pack mass for 21700 lithium-ion, lithium-polymer and lithium iron phosphate, with the four largest observed packs marked. An 840 Wh pack costs 4.9 kg as lithium-ion and 8.4 kg as lithium iron phosphate, so chemistry is a 3.5 kg decision on the mass budget. Sample: manufacturer data for three chemistries and four observed packs.Robotics Club @ Mississippi State University, 2026. Original analysis. S-VENDOR-MOLICEL-P42A-DS S-VENDOR-TATTU-PLUS-16AH Full resolution
Loading chart…

The interactive view plots the eight packs in the data table that publish a nameplate energy, from 320 to 840 Wh. The static figure above shows the six largest of them against the modelled requirement.

Observed capacity runs 1.6 to 3.1 times the single-mission model. Four explanations fit the record better than “teams oversize”: a 120 A peak needs at least three cells in parallel for current alone, a second mission may follow within ten minutes, unmodelled hotel growth (West Virginia’s 2026 rover runs eleven cameras, a 3D lidar, three radios and two computers), and a lithium iron phosphate pack holds about 70 % more mass for the same energy, at 100 Wh/kg against 170 Wh/kg for lithium-ion. UIU’s pack grew from 432 Wh to 840 Wh across five generations while the rover mass stayed flat at 47.5–49.8 kg S-UIU-ROVER-PAGE-AURION S-WVU-SAR2026.

The values on this page

Statistic Value Definition Period Sample Source Chart and chapter
Average draw 249 W Mission-mix mean, 50 kg rover 2027 model 35-minute load table S-URC27-RULES Mass and power
Peak draw 3.7 kW Everything-at-once estimate 2027 model 35-minute load table S-URC27-RULES Power subsystem
Credible peak 156 A, 4.0 kW Climb, stalled arm joint and hotel 2027 model 50 kg rover S-URC27-RULES Chart above; Power subsystem
Delivery energy 145 Wh 50 kg, 60-minute delivery mix 2027 model One mission case S-URC27-RULES Mass and power
Nameplate, one Delivery 273 Wh After 25 % margin and 0.662 usable 2027 One mission case S-URC27-RULES Mass and power data
Nameplate, back-to-back 289 Wh Autonomy then Servicing on one pack 2027 One mission pair S-URC27-RULES Mass and power data
Recommended pack 400–500 Wh 2.4–2.9 kg including BMS and enclosure 2027 First build S-URC27-RULES Power subsystem
Observed packs 320–840 Wh Published nameplate energies 2022–2026 8 packs S-UIU-ROVER-PAGE-AURION S-WVU-SAR2024 Chart above; Mass and power data

Evidence note

Every watt and watt-hour on this page is a model output from a bottom-up load table, not a measurement on a rover. No team publishes a measured energy per mission, so the model cannot be calibrated against the field. Its sensitivity is wide: the 60-minute delivery case ranges from 221 Wh to 410 Wh of nameplate across plausible rolling resistance, efficiency, speed, grade and duration. Duration and speed dominate, which is to say the energy budget is a driving-distance budget in disguise.

Sources for this page

  1. S-URC27-RULESUniversity Rover Challenge 2027 – Requirements and GuidelinesThe Mars Society / URC.Original Archived copy
  2. S-UIU-ROVER-PAGE-AURION5th-gen flagship. Headline specs on the homepage: 47.5 kg total mass (under 50 kg limit), 2.0 m/s max, 6-DOF carbon-fibre manipulator, dual RealS…team (self-published), 2026.Original
  3. S-WVU-SAR2026Team Mountaineers System Acceptance Review 2026 (rover "Deimos"): tri-modal 2.4 GHz + 5.8 GHz + 70 cm, gimbal camera on antenna mast, 750 m LOS / 164 m NLOS high-noise test, antenna + radio budget linesWVU Team Mountaineers, 2026.Original
  4. S-WVU-SAR2024Team Mountaineers System Acceptance Review 2024 (rover "Heimdall"): dual-band 2.4 GHz + 900 MHz, 90°/120° sector antennas, 250 m / 1 km tested, antenna and radio budget linesWVU Team Mountaineers, 2024.Original