top of page

ASTRA-AP

100 Km target altitude 

Mach 5.3

Two-stage architecture

ASTRA-AP is a two-stage hypersonic research rocket designed to reach altitudes above 100 km.
The project combines advanced aerodynamics, high-speed thermal protection studies, robust recovery systems and in-flight data acquisition.
The goal is to push student rocketry toward the edge of near-space flight.

image-removebg-preview (17)_edited.png

The ASTRA-AP project includes a full-scale system test campaign at the Friends of Amateur Rocketry (FAR) launch site in California.

FAR is one of the most emblematic amateur rocketry ranges in the world, used by universities, private teams and experimental aerospace groups to test high-performance rockets in real conditions.

Two-Stage Hypersonic Rocket

Dimensions

  • Length: 3.40 m

  • Configuration: Two-stage rocket

  • Structure: Composite & metallic hybrid airframe

Performance

  • Maximum speed: ~ Mach 5.3

  • Apogee objective: 110+ km

  • Ascent profile: Supersonic → Hypersonic transition

Mission Goals

Hypersonic_Rocket_Cinematic_Render-removebg-preview.png
  • Validating high-altitude flight dynamics

  • Hypersonic aerodynamic behavior

  • Recovery system deployment

  • In-flight data collection

Primary Simulation Tool 

image-removebg-preview (18).png

Designed to Hold Through the Impossible

Eyebolt
A simple shape with a critical role: linking the rocket to its recovery system. Built to stay locked through vibration, acceleration, and hypersonic ascent.


Structural Base
The hidden backbone of the vehicle. It channels tons of force, keeps the motor perfectly aligned, and ensures the entire recovery sequence starts exactly when it should.
Capture_d_écran_2025-11-28_à_09.19.05-removebg-preview.png
Capture_d_écran_2025-11-28_à_09.20.25-removebg-preview.png
Interstage Structure 
A lightweight, aerodynamic link between the two stages.
Engineered to stay rigid through supersonic ascent and release cleanly at booster burnout.


Separation Mechanism
A simple, reliable interface that ensures both stages detach smoothly. Its geometry minimizes drag and resists structural loads during the most intense phase of flight.


Separation Detection 
A straightforward mechanical trigger confirms that the stages have fully detached. The signal synchronizes the ignition sequence of the second stage with perfect timing.

Seeing the Mission. Controlling the Mission.

Onboard Camera
Capturing the ascent, separation, and high-altitude flight in real time.
A lightweight wide-angle camera mounted inside the nosecone provides unique footage from the edge of space.
Capture d’écran 2025-12-03 à 20.43.57.png
Capture d’écran 2025-12-03 à 20.44.37.png

Embedded Electronics

Mission Computer

Sensing Unit

Capture_d_écran_2025-12-03_à_21.45.11-removebg-preview.png
Capture_d_écran_2025-12-03_à_21.45.43-removebg-preview.png
Capture_d_écran_2025-12-03_à_21.58.46-removebg-preview.png
Capture_d_écran_2025-12-03_à_21.58.55-removebg-preview.png

Flight Simulations & Analysis

Stars Leofly

Léofly

leofly@devinci.fr

12 Avenue Léonard de Vinci,

92400 Courbevoie, France

Blog / Articles

Documentation

Photos

Partenaires

Compétitions

Euroc

C'Space

Minif

Smart Wing

Notre Association

Légal

Mentions légales

© 2025 by Eden Elfassy

  • Design_sans_titre_copie-removebg-preview
  • Design_sans_titre-removebg-preview
  • Design_sans_titre__1_-removebg-preview (1)

CGU

Ressources

À propos de Léofly

Données personnelles

Notre équipe

Histoire 

bottom of page