NASA reference study

Orion

crew spacecraft and abort architecture. Architecture: Crew module, European service module, spacecraft adapter, launch abort system.

Use in design study

Orbital visual

Spacecraft mission image

This page includes the generated orbital spacecraft image for capsule, payload, and mission context.

Spacecraft mission image

Vehicle Details

CrewArtemis lunar crew spacecraft
Abort systemtower with abort, attitude-control, and jettison motors
Mission classdeep-space crew transport
Launch vehicleSLS for Artemis missions
Safety focusrapid crew escape during pad/ascent emergency

AeroVectrix Study Notes

  • Orion is not a rocket booster; it is included for crew safety, abort modes, service-module design, and re-entry architecture.
  • AeroVectrix study focus: abort envelopes, human-rating documentation, parachute recovery, service module interfaces, and crew survival systems.

Working Model

Ascent

Mission begins with thrust-to-weight margin, guidance through dense atmosphere, max-Q load management, and staging when the lower stage has delivered useful impulse.

Staging

Separation events must protect vehicle attitude, avoid recontact, confirm engine start conditions, and preserve payload environment limits.

Mission Assurance

Public vehicle studies should track assumptions, review dates, risk areas, and unknowns rather than overclaim exact proprietary data.