Meet Daytona I
Booking Launches for 2025
MASS TO LOW EARTH ORBIT
LIFTOFF THRUST OF DAYTONA I LAUNCH VEHICLE
PRICE ($M) PER DEDICATED DAYTONA LAUNCH
Daytona I
Specifications
PAYLOAD TO 500 km CIRCULAR SUN SYNCHRONOUS ORBIT (SSO): 53 kg (117 lbs)
18 m (59 ft)
HEIGHT
1.5 M (4.9 FT)
DIAMETER
Meet our first launch vehicle
Daytona I 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. Mass manufacturing techniques allow Daytona to be the most efficient and cost-effective small payload rocket in the world.
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.
Length
2.3 m / 7.5 ft
Diameter
1.4 m / 4.6 ft
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).
Diameter
1.5 m / 4.9 ft
Thrust
200 kN / 45,000 lbf
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.
Diameter
1.5 m / 4.9 ft
Thrust
28.8 kN / 6470 lbf
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
22.2 kN / 5000 lbf
Vacuum Thrust
28.8 kN / 6470 lbf
