| Closest approach | 54.6 million km |
| Farthest distance | 401 million km |
| Distance range | 7.3× variation |
| One-way light time | 3 – 22 minutes |
| Synodic period | 779.94 days (26 months) |
| TCP/IP expects | Deep-space reality |
|---|---|
| RTT < 200 ms | 6 – 44 min RTT |
| Always connected | Scheduled contacts only |
| End-to-end path | No simultaneous route |
| ACKs in seconds | ACKs take minutes–hours |
| P0 EMERGENCY | Life-critical alerts, abort |
| P1 URGENT | Nav corrections, hazards |
| P2 NORMAL | Telemetry, science, commands |
| P3 LOW | Software updates, bulk files |
| P4 BULK | Background sync, archival |
| Tier | Nodes | Assets |
|---|---|---|
| T1 Earth Ground | 5 | 3 DSN (Goldstone, Madrid, Canberra) + MOC + SOC |
| T2 Earth Orbital | 51 | 3 GEO + 48 LEO laser mesh |
| T3 Deep Space | 4 | ES-L4, ES-L5 + 2 transfer-orbit relays |
| T4 Mars Orbital | 4 | 2 areostationary + 1 polar + 1 orbiter |
| T5 Mars Surface | 177 | 2 bases, 5 rovers, 10 drones, 160 sensors |
| Total | 241 |
| Link | Rate | Type |
|---|---|---|
| Earth ↔ Deep Space | 100 Mbps | 1550 nm optical |
| Deep Space ↔ Mars | 2–200 Mbps | distance-dependent |
| Mars Orbit ↔ Surface | 2 Mbps | UHF / X-band |
| LEO inter-satellite | 10 Gbps | optical ISL |
| Wavelength | 1550 nm (telecom heritage) |
| Tx power | 5 W |
| Tx aperture | 22 cm |
| Rx aperture | 5.0 m (Hale-class ground) |
| Phase | Protocol | Key rate |
|---|---|---|
| 1 — LEO | BB84 | 1–10 kbps |
| 2 — GEO | BB84 + E91 | 10–100 kbps |
| 3 — Mars | E91 + repeaters | 1+ kbps |
| Semi-major axis | 1.524 AU |
| Synodic period | 779.94 days |
| Distance range | 54.6M – 401M km |
| Areostationary alt. | 17,032 km |
| Doppler (Ka, max) | ±2.1 MHz @ 24 km/s |
| Window | Avail. | Duration | Rate |
|---|---|---|---|
| Optimal | 99% | 8–12 hrs | 100–200 Mbps |
| Good | 95% | 6–8 hrs | 20–100 Mbps |
| Fair | 85% | 4–6 hrs | 5–20 Mbps |
| Blackout | 0% | 2–4 wks | — |
| Effect | Mitigation |
|---|---|
| SEU (bit flip) | SECDED ECC |
| MBU (adjacent bits) | Bit interleaving |
| SEL (latch-up) | Current limit + power-cycle |
| TID (cumulative dose) | Rad-hard parts (RAD750) [18] |
| Tier | Class | Examples |
|---|---|---|
| P0 | Emergency | Health, collision, faults |
| P1 | Mission-critical | Command ACKs, time-sensitive sci |
| P2 | High | Routine telemetry, scheduled sci |
| P4 | Bulk | Housekeeping, files, SW images |
| Metric | Current (MRO) [1] | AETHERIX [A4] | Note |
|---|---|---|---|
| Downlink rate | 0.5–6 Mbps | 2–200 Mbps | 10–100× capability |
| Availability | 60–75% | >95% | design target |
| Routing | Static (CGR) | RL-adaptive | autonomous [A1] |
| Security | AES-256 | QKD + PQC | future-proof [16][17] |
| Scalability | 5–10 assets | 241 nodes | 10–100× [A2] |
| Conjunction | Blackout | L4/L5 relay (target) | +50–70% (target) [A8] |
| RFC 9171 | Bundle Protocol v7 |
| RFC 4838 / 5326 / 7242 | DTN / LTP / TCPCL |
| RFC 9172 | BPSec (security) |
| CCSDS 734.2 / 734.3 | Bundle Protocol / SABR |
| CCSDS 141.0-B-1 | Optical comms physical |
| Decision | Choice | Rationale vs alternative |
|---|---|---|
| Optical vs RF | Hybrid 1550 nm + Ka fallback [4] | 10–100× throughput [A4]; RF survives clouds & corona |
| Routing | Custom Q-learning, not ION-DTN CGR [A1] | Adapts to live state; CGR re-plans on stale schedule |
| RL model | Q-tables now, DQN later | Every value auditable; trains in seconds |
| Reward weights | α=1.0, δ=10.0, ε-decay 0.995 [A1] | Drop penalty 10× delivery — forbids bundle loss |
| Path | Band | Quality | Status | Reward [A8] |
|---|---|---|---|---|
| Direct Mars → Earth | 1550 nm optical | 0.05 | CLOSED | −1.438 |
| Mars → ES-L4 → Earth | Ka-band RF | 0.65 | OPEN | −0.201 |
| Mars → ES-L5 → Earth | Ka-band RF | 0.60 | OPEN | −0.201 |