Uptime 15,364 days - The Computers of Voyager
summary
Voyager 1 and 2 continue returning telemetry after 15,364 days (launched 1977) using three core computers — CCS, AACS and the faster CMOS Flight Data System — and survive on three RTGs that produced about 450 watts at launch from 13.5 kg of plutonium‑238. Systems use plated‑wire memory, an 18‑bit bipolar CCS (~11k instr/s), an 80k‑instr/s CMOS FDS, an eight‑track tape holding ~500 megabits (~100 full images), Golay and Reed‑Solomon FEC and runtime reconfiguration; power limits predict roughly five more years of operation.
AI-written summary · about
chapters (16)
- 0:00Background on Voyager
- 1:16Talk outline
- 2:00About the speaker
- 2:25Origins of Voyager
- 3:18Initial requirements
- 8:25Revised program
- 10:05The 3 R's
- 11:08Probe design
- 12:55Command Computer System
- 17:40Attitude and Articulation Control System
- 20:04Flight Data System
- 23:56Voyager 0
- 24:35Voyager 2 mission
- 29:07Sustaining power
- 30:26The golden record
- 31:20Q&A
related talks
49mThe Charming Genius of the Apollo Guidance Computer
59mSockets, Sparks, and Magic Smoke
49mHARDWARE in SPACE! The Kernel at the Edge of the Universe
40mAn Average Working Day on Visionary NASA Projects
50mAn Average Working Day on Visionary NASA Projects
01h 07mContrasting Embedded Software Development for the Space Shuttle and the Orion MPCV
01h 00mIntermittent Computer Systems on Earth and in Space
50mSoftware archaeology - Learning from the landing on the moon!
