MEET
DAYTONA

Daytona Specifications

DIAMETER 1.5 m / 4.9 ft

/

PAYLOAD TO LEO 450 kg / 990 lb

17.8 M / 58.5 FT

HEIGHT

17,900 KG / 39,380 LB

MASS GLOW

Meet our first workhorse launch vehicle

Daytona is a mass manufactured expendable two-stage rocket designed and manufactured by Phantom Space, capable of reliable transport of satellites and other space cargo into Earth orbit and beyond. Mass manufacturing techniques allow Daytona to be the most efficient and cost-effective small payload rocket in the world.

The fairing is designed to protect satellites and spacecraft on their way to orbit.We support a wide variety of payloads, from cube sats to ESPA class satellites or any other custom spacecraft.

Payload

The fairing is designed to protect satellites and spacecraft on their way to orbit.We support a wide variety of payloads, from cube sats to ESPA class satellites or any other custom spacecraft.

Height

3 m / 10 ft

Diameter

1.5 m / 4.9 ft

The first stage utilizes 9 Hadley engines to power the first part of the journey into space. Hadley is powered by liquid oxygen (LOX) and rocket propellant (RP-1).

First Stage

The first stage utilizes 9 Hadley engines to power the first part of the journey into space. Hadley is powered by liquid oxygen (LOX) and rocket propellant (RP-1).

Height

11.8 m / 38.8 ft

Diameter

1.5 m / 4.9 ft

Thrust

200 kN / 45000 lbf

Shortly after first stage separation, the second stage ignites to bring Daytona into orbit.

The second stage uses a single vacuum-optimized Hadley engine, and contains the avionics and all necessary computing required to travel to, through, and back from space.

Second Stage

Shortly after first stage separation, the second stage ignites to bring Daytona into orbit. The second stage uses a single vacuum-optimized Hadley engine, and contains the avionics and all necessary computing required to travel to, through, and back from space.

Height

5.8 m / 19 ft

Diameter

1.5 m / 4.9 ft

Thrust

28.8 kN / 6470 lbf

The Hadley, developed by Ursa Major, is a pump-fed, ultra-high-efficiency, 3D-printed rocket engine fueled by liquid oxygen (LOX) and rocket propellant (RP-1).

Engine

The Hadley, developed by Ursa Major, is a pump-fed, ultra-high-efficiency, 3D-printed rocket engine fueled by liquid oxygen (LOX) and rocket propellant (RP-1).

Propellant

LOX / RP-1

Sea Level Thrust

26.4 kN / 5930 lbf

Vacuum Thrust

28.8 kN / 6470 lbf