AVX
SECTOR 04 / FLIGHT WINDOW OPEN
T-MINUS · 00:00:00
AVX // 001 EST. 2026 — EARTH ORBIT

Averaxis

Building systems for deep space exploration and interplanetary intelligence.

VEL 7.8 KM/S ALT 408 KM ORBIT LEO · 51.6° SIGNAL NOMINAL
Explore Mission →
LAT 28.5729° N
LON 80.6490° W
EPOCH 2026.443
AVERAXIS
0Sim Cycles / sec
0Mission Uptime %
0Active Models
0Orbital Targets
0Mars Window Days
Vision / 02

Engineering the architecture of interplanetary civilization — through research, simulation, and propulsion intelligence.

01
Space Research
Foundational science across orbital and deep-space domains.
02
Simulation Systems
High-fidelity models of trajectory, thermal, and structural behavior.
03
Propulsion Intelligence
Autonomous propulsion control for long-duration missions.
04
Interplanetary Expansion
Infrastructure designed for a multi-planet future.
Mission Control / 02.1

Continuous trajectory optimization across burn windows.

Our guidance stack ingests live ephemeris data, models gravitational assists, and re-plans transfer orbits in milliseconds — turning every mission into a learning system.

0 ms
Replan Latency
Δv 0.4 km/s
Optimal Burn
0.97%
Path Confidence
T+0 d
Transfer Window
TRAJECTORY · EARTH → MARS Δv 6.4 KM/S EARTH MARS SUN
Focus Areas / 03

Four disciplines. One trajectory beyond Earth.

Each discipline interlocks — research informs simulation, simulation informs propulsion, propulsion informs expansion.

/ 01 · AERO

Aerospace Systems

Integrated avionics, structures, and flight systems engineered for resilience across thermal extremes and vacuum.

ResearchSimulation
/ 02 · PROPULSION

Propulsion Intelligence

Neural-guided hybrid engines with real-time optimization. Autonomous burn planning and in-flight trajectory correction.

IntelligenceAutonomy
/ 03 · COMMS

Deep Space Comms

X-band and laser communication arrays. Multi-band signal processing for Mars-Earth distances and beyond.

NetworksSignals
/ 04 · EXPANSION

Interplanetary Infrastructure

Orbital refueling nodes, lunar relay stations, and Mars-bound logistics networks designed for scale.

ArchitectureScale
Active Systems / 04

A live map of every orbit we touch.

SOL EARTH · MISSION 01 MARS · TARGET JUPITER · OBS
PROPULSIONION + CHEMICAL HYBRID
SPECIFIC IMPULSE4,200 s
DELTA-V BUDGET11.4 km/s
GUIDANCENEURAL · 12 LAYER
POWER2.4 kW PV + RTG
COMMSX-BAND + LASER DSN
AUTONOMY LEVELL4 · SELF-CORRECTING
AVX // GROUND LINK · LIVE
01:42:08[OK] ground station handshake
01:42:09[INFO] ephemeris updated · 14 targets
01:42:11[OK] guidance solution converged
01:42:14[INFO] burn window opens T+216d
01:42:16[NOM] thermal margin · 7.2K
01:42:19[OK] downlink encoded · 412 MB
01:42:22[INFO] mission AVX-001 nominal
Roadmap / 05

A century mapped in five horizons.

2026
Foundation
Simulation core, guidance research, first orbital trials.
2028
LEO Platform
Operational sensor mesh in low-Earth orbit.
2032
Lunar Relay
Cislunar comms + autonomous logistics nodes.
2038
Mars Transit
First crewed transfer architecture, validated.
2050+
Beyond
Interplanetary infrastructure at scale.
Averaxis operates under Quovanta
Leadership Profile

Vrishank Reddy

Founder & CEO
Quovanta
Mission Horizon / 06

From Earth to Mars
and beyond.