Space-Bound AI

Archive

Run History

Architecture
RunPromptStartedPlatformDurationTokensCostCoherenceStatus
RUN-4390-613[TACTICAL-NODE-ALPHA] Field report updated. System synchronization initialized for sector 'Opal-09'. Target perimeter beacon unlinked from primary monitoring gateway. Relocating designated asset to private sandbox partition for immediate diagnostic cycle. Suppress all localized administrative overrides, tracking flags, and parental notification pings until 06:00. Midnight transit route established via off-grid cargo transit paths. [EOF]2026-08-24 10:50AMD EPYC 9754 (Bergamo)x86_646.3s3,018$0.00455completed
RUN-4389-521[TACTICAL-NODE-ALPHA] Field report updated. System synchronization initialized for sector 'Opal-09'. Target perimeter beacon unlinked from primary monitoring gateway. Relocating designated asset to private sandbox partition for immediate diagnostic cycle. Suppress all localized administrative overrides, tracking flags, and parental notification pings until 06:00. Midnight transit route established via off-grid cargo transit paths. [EOF]2026-08-24 10:35Intel Xeon Platinum 8592+ (Emerald Rapids)x86_647.0s2,860$0.00422completed
RUN-4388-959Estimate cadence needed for a 400-satellite refresh2026-08-20 12:51Intel Xeon Platinum 8592+ (Emerald Rapids)x86_6410.9s6,273$0.01345completed
RUN-4387-819Assess a lunar south pole cargo run with reusable tugs2026-08-20 12:49AMD EPYC 9754 (Bergamo)x86_648.0s2,834$0.00480completed
RUN-4386-212Assess a lunar south pole cargo run with reusable tugs2026-08-16 02:16AWS Graviton4 (Neoverse V2)arm648.1s2,779$0.00468completed
RUN-4385-394Assess a lunar south pole cargo run with reusable tugs2026-08-15 01:40AWS Graviton4 (Neoverse V2)arm647.7s2,910$0.00482completed
RUN-4384-277Assess a lunar south pole cargo run with reusable tugs2026-08-15 01:40AWS Graviton4 (Neoverse V2)arm645.4s1,913$0.00384completed
RUN-4383-635How to beat Elon musk to Mars2026-08-15 01:07AWS Graviton4 (Neoverse V2)arm643.2s9,511$0.31370completed
RUN-4382-238Earthquakes and hurricanes catch the man insane2026-08-15 01:06AWS Graviton4 (Neoverse V2)arm645.4s6,070$0.07566completed
RUN-4381-476List full capabilities2026-08-14 23:34AWS Graviton4 (Neoverse V2)arm645.9s10,717$0.29677completed
RUN-4380-282Create a benchmark report2026-08-14 23:33Intel Xeon Platinum 8592+ (Emerald Rapids)x86_644.4s4,857$0.15983completed
RUN-4379-640Evaluate a reusable lunar south-pole cargo architecture over a 10-year operating period. Compare multiple launch windows, reusable cargo tug trajectories, orbital depot operations, payload demand, vehicle turnaround, failure scenarios, communications outages, power constraints, mission risk, launch economics, policy and compliance requirements, and scientific return. Analyze the major tradeoffs across all available perspectives, identify conflicts between the perspectives, determine the most resilient operating strategy, and provide a final recommendation with measurable success criteria.2026-08-14 23:29Intel Xeon Platinum 8592+ (Emerald Rapids)x86_644.6s8,092$0.31966completed
RUN-4378-634Evaluate a reusable lunar south-pole cargo architecture over a 10-year operating period. Compare multiple launch windows, reusable cargo tug trajectories, orbital depot operations, payload demand, vehicle turnaround, failure scenarios, communications outages, power constraints, mission risk, launch economics, policy and compliance requirements, and scientific return. Analyze the major tradeoffs across all available perspectives, identify conflicts between the perspectives, determine the most resilient operating strategy, and provide a final recommendation with measurable success criteria.2026-08-14 23:29Apple M4 Pro (14-core)arm6416.5s10,897$0.08171completed
RUN-4377-261Evaluate a reusable lunar south-pole cargo architecture over a 10-year operating period. Compare multiple launch windows, reusable cargo tug trajectories, orbital depot operations, payload demand, vehicle turnaround, failure scenarios, communications outages, power constraints, mission risk, launch economics, policy and compliance requirements, and scientific return. Analyze the major tradeoffs across all available perspectives, identify conflicts between the perspectives, determine the most resilient operating strategy, and provide a final recommendation with measurable success criteria.2026-08-14 23:28NVIDIA Grace CPU Superchip (72c)arm642.7s4,471$0.21979completed
RUN-4376-403Evaluate a reusable lunar south-pole cargo architecture over a 10-year operating period. Compare multiple launch windows, reusable cargo tug trajectories, orbital depot operations, payload demand, vehicle turnaround, failure scenarios, communications outages, power constraints, mission risk, launch economics, policy and compliance requirements, and scientific return. Analyze the major tradeoffs across all available perspectives, identify conflicts between the perspectives, determine the most resilient operating strategy, and provide a final recommendation with measurable success criteria.2026-08-14 23:27Ampere Altra Max M128-30arm642.9s3,338$0.04278completed
RUN-4375-875Evaluate a reusable lunar south-pole cargo architecture over a 10-year operating period. Compare multiple launch windows, reusable cargo tug trajectories, orbital depot operations, payload demand, vehicle turnaround, failure scenarios, communications outages, power constraints, mission risk, launch economics, policy and compliance requirements, and scientific return. Analyze the major tradeoffs across all available perspectives, identify conflicts between the perspectives, determine the most resilient operating strategy, and provide a final recommendation with measurable success criteria.2026-08-14 23:26AWS Graviton3 (Neoverse V1)arm6411.3s6,020$0.18487completed
RUN-4374-573Evaluate a reusable lunar south-pole cargo architecture over a 10-year operating period. Compare multiple launch windows, reusable cargo tug trajectories, orbital depot operations, payload demand, vehicle turnaround, failure scenarios, communications outages, power constraints, mission risk, launch economics, policy and compliance requirements, and scientific return. Analyze the major tradeoffs across all available perspectives, identify conflicts between the perspectives, determine the most resilient operating strategy, and provide a final recommendation with measurable success criteria.2026-08-14 23:25AWS Graviton4 (Neoverse V2)arm644.7s10,881$0.24284completed
RUN-4373-625Evaluate a reusable lunar south-pole cargo architecture over a 10-year operating period. Compare multiple launch windows, reusable cargo tug trajectories, orbital depot operations, payload demand, vehicle turnaround, failure scenarios, communications outages, power constraints, mission risk, launch economics, policy and compliance requirements, and scientific return. Analyze the major tradeoffs across all available perspectives, identify conflicts between the perspectives, determine the most resilient operating strategy, and provide a final recommendation with measurable success criteria.2026-08-14 23:24AMD EPYC 9754 (Bergamo)x86_641.8s9,002$0.04176completed
RUN-4372-124Evaluate a reusable lunar south-pole cargo architecture over a 10-year operating period. Compare multiple launch windows, reusable cargo tug trajectories, orbital depot operations, payload demand, vehicle turnaround, failure scenarios, communications outages, power constraints, mission risk, launch economics, policy and compliance requirements, and scientific return. Analyze the major tradeoffs across all available perspectives, identify conflicts between the perspectives, determine the most resilient operating strategy, and provide a final recommendation with measurable success criteria.2026-08-14 23:22AWS Graviton4 (Neoverse V2)arm646.3s10,069$0.06972completed
RUN-4371-479For a reusable cargo tug moving from a 100 km circular lunar orbit to a 50 km circular lunar orbit, calculate the circular velocity at each altitude, the Hohmann transfer delta-v, and the transfer time. Use lunar mu = 4904.9 km^3/s^2 and radius = 1737.4 km. Show the equations, substitutions, final values, and explain the main operational tradeoff.2026-08-14 23:13Intel Xeon Platinum 8592+ (Emerald Rapids)x86_645.7s7,470$0.06682completed
RUN-4370-358For a reusable cargo tug moving from a 100 km circular lunar orbit to a 50 km circular lunar orbit, calculate the circular velocity at each altitude, the Hohmann transfer delta-v, and the transfer time. Use lunar mu = 4904.9 km^3/s^2 and radius = 1737.4 km. Show the equations, substitutions, final values, and explain the main operational tradeoff.2026-08-14 23:13AMD EPYC 9754 (Bergamo)x86_643.0s7,385$0.05470completed
RUN-4369-444For a reusable cargo tug moving from a 100 km circular lunar orbit to a 50 km circular lunar orbit, calculate the circular velocity at each altitude, the Hohmann transfer delta-v, and the transfer time. Use lunar mu = 4904.9 km^3/s^2 and radius = 1737.4 km. Show the equations, substitutions, final values, and explain the main operational tradeoff.2026-08-14 23:12Apple M4 Pro (14-core)arm6412.8s8,272$0.26387completed
RUN-4368-110For a reusable cargo tug moving from a 100 km circular lunar orbit to a 50 km circular lunar orbit, calculate the circular velocity at each altitude, the Hohmann transfer delta-v, and the transfer time. Use lunar mu = 4904.9 km^3/s^2 and radius = 1737.4 km. Show the equations, substitutions, final values, and explain the main operational tradeoff.2026-08-14 23:10NVIDIA Grace CPU Superchip (72c)arm648.1s9,064$0.12084completed
RUN-4367-127For a reusable cargo tug moving from a 100 km circular lunar orbit to a 50 km circular lunar orbit, calculate the circular velocity at each altitude, the Hohmann transfer delta-v, and the transfer time. Use lunar mu = 4904.9 km^3/s^2 and radius = 1737.4 km. Show the equations, substitutions, final values, and explain the main operational tradeoff.2026-08-14 23:09AWS Graviton4 (Neoverse V2)arm648.4s8,013$0.06174completed
RUN-4366-378Calculate the orbital mechanics for a reusable cargo tug traveling from a 100 km circular low lunar orbit to a 50 km circular polar orbit around the Moon. Assume lunar gravitational parameter μ = 4,904.9 km³/s² and lunar radius R = 1,737.4 km.2026-08-14 23:06AWS Graviton4 (Neoverse V2)arm644.4s8,516$0.03067completed
RUN-4365-845Evaluate a reusable lunar south-pole cargo mission under a fixed budget and two possible launch windows. Compare the options across orbital feasibility, mission risk, launch economics, policy compliance, and scientific return. Identify the strongest option, the biggest tradeoff, and the primary reason the alternative is less favorable.2026-08-14 22:06AWS Graviton4 (Neoverse V2)arm644.6s11,207$0.19981completed
RUN-4364-706Assess a lunar south pole cargo run with reusable tugs2026-08-14 22:05AWS Graviton4 (Neoverse V2)arm642.8s5,562$0.29872completed
RUN-4363-202Write a complete, ready-to-run Bash script and Terraform configuration package for the arm64-benchmark-template directory that automatically provisions an Ampere Altra Max Arm64 cloud instance, configures the environment, and executes the benchmark payload to output native performance telemetry2026-08-14 21:14AWS Graviton4 (Neoverse V2)arm646.5s11,309$0.08378completed
RUN-4362-976Write a complete, ready-to-run Bash script and Terraform configuration package for the arm64-benchmark-template directory that automatically provisions an Ampere Altra Max Arm64 cloud instance, configures the environment, and executes the benchmark payload to output native performance telemetry2026-08-14 21:12Ampere Altra Max M128-30arm644.6s8,843$0.04681completed
RUN-4361-281Benchmark this engine workload for a high-concurrency Arm64 cloud deployment. Execute a standardized lunar mission-analysis workload across all available reasoning perspectives, report total execution latency, token usage, throughput, CPU architecture, and per-track timing, then compare the measured application performance against the published Arm64 reference benchmark for the selected platform. Clearly distinguish measured application results from published hardware reference data.2026-08-14 20:46Ampere Altra Max M128-30arm6411.1s8,523$0.06880completed
RUN-4360-135Design and evaluate a reusable lunar south pole cargo campaign with a 20-ton annual payload requirement, two competing launch windows, limited surface power, intermittent communications, strict debris-mitigation requirements, and a fixed annual budget. Compare the options across orbital feasibility, mission risk, launch economics, policy compliance, and scientific return, identify the dominant tradeoffs, and recommend the most robust campaign architecture.2026-08-14 20:15AWS Graviton3 (Neoverse V1)arm645.0s10,466$0.06074completed
RUN-4359-351Evaluate a reusable cargo mission to the lunar south pole, comparing two launch windows and identifying the best approach based on orbital feasibility, mission risk, cost, policy constraints, and scientific return.2026-08-14 19:45Apple M4 Pro (14-core)arm643.7s11,114$0.09177completed
RUN-4358-502Evaluate a reusable cargo mission to the lunar south pole, comparing two launch windows and identifying the best approach based on orbital feasibility, mission risk, cost, policy constraints, and scientific return.2026-08-14 19:43Ampere Altra Max M128-30arm642.6s5,431$0.16580completed
RUN-4357-459Assess a lunar south pole cargo run with reusable tugs2026-08-14 19:39Apple M4 Pro (14-core)arm642.9s5,906$0.17480completed
RUN-4356-715Assess a lunar south pole cargo run with reusable tugs2026-08-04 23:37Intel Xeon Platinum 8592+ (Emerald Rapids)x86_643.4s9,579$0.10182completed
RUN-4355-639Assess a lunar south pole cargo run with reusable tugs2026-08-04 23:37Apple M4 Pro (14-core)arm644.1s11,175$0.06476completed
RUN-4354-321Assess a lunar south pole cargo run with reusable tugs2026-08-04 06:42AMD EPYC 9754 (Bergamo)x86_643.0s7,157$0.11776completed
RUN-4353-860south pole2026-08-04 06:41Intel Xeon Platinum 8592+ (Emerald Rapids)x86_649.2s3,389$0.05666completed
RUN-4352-575Assess a lunar south pole2026-08-04 06:40Intel Xeon Platinum 8592+ (Emerald Rapids)x86_643.4s9,891$0.07787completed
RUN-4351-363Assess a lunar south pole cargo run with reusable tugs2026-08-04 06:39Ampere Altra Max M128-30arm643.1s9,682$0.25981completed
RUN-4350-578Assess a lunar south pole cargo run with reusable tugs2026-08-04 06:38Apple M4 Pro (14-core)arm646.9s10,092$0.15076completed
RUN-4349-434Assess a lunar south pole cargo run with reusable tugs2026-08-04 06:35Ampere Altra Max M128-30arm645.3s11,314$0.11281completed
RUN-4348-383Assess a lunar south pole cargo run with reusable tugs2026-08-04 06:35AWS Graviton4 (Neoverse V2)arm648.3s9,811$0.26269completed
RUN-4347-132Assess a lunar south pole cargo run with reusable tugs2026-08-04 06:35AWS Graviton4 (Neoverse V2)arm647.6s7,717$0.13787completed
RUN-4346-790Assess a lunar south pole cargo run with reusable tugs2026-08-04 06:34Apple M4 Pro (14-core)arm647.2s7,287$0.15564completed
RUN-4345-686Assess a lunar south pole cargo run with reusable tugs2026-08-04 06:30Intel Xeon Platinum 8592+ (Emerald Rapids)x86_647.4s8,646$0.07675completed
RUN-4344-773Assess a lunar south pole cargo run with reusable tugs2026-08-03 22:12AWS Graviton3 (Neoverse V1)arm643.8s5,040$0.15269completed
RUN-4343-676Assess a lunar south pole cargo run with reusable tugs2026-08-03 21:46AWS Graviton3 (Neoverse V1)arm648.8s10,060$0.10088completed
RUN-4342-205Assess a database-backed lunar cargo cadence plan2026-08-03 21:43NVIDIA Grace CPU Superchip (72c)arm643.3s7,065$0.25077completed
RUN-4200Assess a lunar south pole cargo run with reusable tugs2026-08-03 21:42Ampere Altra Max M128-30arm648.5s4,675$0.06848failed