Go Back

Launch details STP-2

No description provided

Description: Space Test Program 2 is a rideshare managed by the U.S. Air Force Space and Missile Systems Center (SMC), launching from LC-39A, KSC. Most of the spacecraft will be delivered into low Earth orbit (LEO) in two deployment sequences separated by a second stage burn. These LEO payloads include the six Taiwan and United States owned COSMIC-2 microsatellites, the Planetary Society's LightSail-B demonstrator cubesat, and others. The third and final deployment will be the Air Force Research Lab's DSX spacecraft, which will be delivered to a medium Earth orbit (MEO). This mission will reuse the side cores from Arabsat 6A, which will return to LZ-1, and LZ-2. The new center core will boost back to land on OCISLY less than 40 km from the launch site.

- Information:

  • Flight number: 81
  • Flight date: 6/25/2019
  • Static fire: 6/19/2019
  • Status: Exitoso
Logo del lanzamiento STP-2

Information:

State: Active

Company: SpaceX

First Flight: 2018-02-06

Country: United States

Success Rate: 100%

Description: With the ability to lift into orbit over 54 metric tons (119,000 lb)--a mass equivalent to a 737 jetliner loaded with passengers, crew, luggage and fuel--Falcon Heavy can lift more than twice the payload of the next closest operational vehicle, the Delta IV Heavy, at one-third the cost.

Details:

- Rocket Details:

  • Height: 70 meters / 229.6 feet
  • Diameter: 12.2 meters / 39.9 feet
  • Mass: 1420788 kg / 3125735 lb
  • Stages: 2
  • Boosters: 2
  • Cost per Launch: $90000000

- Engines:

  • Type: merlin
  • Version: 1D+
  • Layout: octaweb
  • Thrust vacuum:
  • Engine Loss Max: 6
  • Propellant 1: liquid oxygen
  • Propellant 2: RP-1 kerosene
  • Thrust to Weight: 180.1

- Payload Weights:

  • Low Earth Orbit: 63800 kg / 140660 lb
  • Geosynchronous Transfer Orbit: 26700 kg / 58860 lb
  • Mars Orbit: 16800 kg / 37040 lb
  • Pluto Orbit: 3500 kg / 7720 lb

- Landing Legs:

  • Number: 12
  • Material: carbon fiber

First and Second Stage

Stage Thrust vacuum kN/lbf Reusable Engines Fuel Amount Tons Burn Time Sec
1 24681 / 5548500 Yes 27 1155 tons 162 sec
2 934 / 210000 Yes 1 90 tons 397 sec

- Rocket gallery

Image rocket 1
Image rocket 2
Image rocket 3
Image rocket 4