Independent aircraft concept · 01 / 07

Regional flight,
reimagined.

Meet SKYWARD: a study in quieter, cleaner connections between the places that need them most.

DESIGN STATUSEarly-stage concept · Not flight tested
SW–01 / THREE-QUARTER VIEW SKYWARD concept aircraft An original technical illustration of a small, high-wing regional aircraft with distributed electric propulsors. CONCEPTUAL STUDY · NOT TO SCALECONFIGURATION A
SW–01Distributed electric propulsors
A DESIGN STUDY IN PROGRESS Scroll to explore 39°44' N — 104°59' W

01 / Concept

A better connection
starts between cities.

Regional journeys are often too long for the road and too short for the airport. SKYWARD explores a purpose-built aircraft for that in-between distance—designed around flexibility, efficiency, and a lighter footprint.

DESIGN INTENTConnect communities

Explore practical regional links beyond major hubs.

DESIGN APPROACHElectric-first study

Investigate distributed propulsion at concept level.

PROJECT PHASEFeasibility & layout

Early design exploration; no aircraft has been built.

02 / Aircraft

One airframe.
Five design lenses.

A preliminary configuration to make the design conversation concrete. These are illustrative assumptions—not measured, validated, or certified aircraft data.

CONFIGURATION / A

Purpose-sized
for regional routes.

High-wing, pressurized-cabin concept with a notional 19-seat layout. The preliminary configuration favors short-field access and distributed electric propulsion as topics for future study.

All figures are illustrative concept targets, not real measurements.
DESIGN PARAMETERSCONCEPT ONLY
Passenger capacity
19 seats target
Design range
400 nmi study target
Configuration
High wing preliminary
Propulsion
Distributed electric under study
Operating role
Regional transport concept

Not engineering specifications. No performance, safety, or certification claim is implied.

02 / CABIN + AIRFRAME

Layout

A high-wing cabin layout keeps the floor clear for boarding and luggage. A 19-seat arrangement is a packaging study, not a finalized interior.

03 / FLOW STUDY

Aerodynamics

High-aspect-ratio wing and propeller–wing interaction are design questions for analysis, not claimed performance advantages.

ILLUSTRATIVE FLOW · NOT CFD RESULTS
04 / POWERTRAIN STUDY

Propulsion

Distributed electric propulsors are a concept direction. Energy storage, thermal management, redundancy, and dispatch reliability remain open engineering challenges.

Energy
storage
Power
electronics
Electric
motors
ARCHITECTURE UNDER STUDY · NO POWER RATINGS
05 / STRUCTURAL APPROACH

Structure

Conventional semi-monocoque fuselage and a high-wing primary structure provide a starting point for load-path and maintainability studies.

Wing box
Fuselage
Landing gear
DESIGN TOPICS ONLY · NO LOAD ANALYSIS

03 / Performance

Targets that
invite better questions.

Concept-stage goals help shape the study. They are not calculated outputs, guaranteed capabilities, or certified limits.

How we plan to evaluate them
01
Short regional sectors

Explore routes connecting smaller communities.

MISSION AIM
02
Reduced local noise

Assess distributed propulsion and community impact.

STUDY AREA
03
Useful 19-seat cabin

Test practical passenger and baggage packaging.

LAYOUT TARGET
04
Lower-emission operation

Compare energy pathways over a representative mission.

OPEN QUESTION

Concept goals only. Actual performance depends on validated design, operating conditions, and certification.

04 / Simulation

From sketch to
evidence.

A simulation plan for turning design questions into traceable analysis. No computational results are presented as completed work.

01AERODYNAMICS

Geometry & flow

Build a consistent baseline model; establish mesh, boundary conditions, and convergence checks before comparing configurations.

PLANNED WORK
02MISSION ENERGY

Power & range

Model mission segments, energy use, reserves, and sensitivities with explicit assumptions and realistic system losses.

PLANNED WORK
03STRUCTURES

Loads & margins

Map preliminary load cases and identify where detailed structural analysis and independent review are required.

PLANNED WORK

05 / Development

Good aircraft
design is iterative.

A transparent path from mission definition to a reviewable preliminary design, with assumptions made visible at every stage.

  1. PHASE 01

    Define the mission

    Identify the regional use case, passenger needs, and initial constraints.

    IN PROGRESS
  2. PHASE 02

    Explore configuration

    Compare airframe, cabin, and propulsion layouts against the mission.

    NEXT
  3. PHASE 03

    Build analysis models

    Document methods, validate inputs, then run focused simulations.

    PLANNED
  4. PHASE 04

    Review & refine

    Use evidence and expert review to revise open design decisions.

    PLANNED

06 / Documentation

A living record
of the design.

Design decisions, assumptions, and planned analyses belong in the open. The brief below summarizes the current concept and its limitations.

Read the concept brief
01Concept overview↗ 02Preliminary specifications↗ 03Analysis plan↗ 04Development roadmap↗

All numerical targets and technical descriptions on this site are illustrative, conceptual assumptions. SKYWARD is not a real, built, tested, or certified aircraft. Nothing here should be used for operational, engineering, or safety decisions.