Long March 1 Rocket - Chinese Launch Systems

Long March 1 Rocket

The Long March 1 (长征一号), also known as Changzheng-1 (CZ-1), was China‘s inaugural orbital launch vehicle and the first in the Long March rocket family. Developed in the 1960s, it was derived from the Dong Feng 4 (DF-4) intermediate-range ballistic missile, modified with an additional third stage to achieve the necessary velocity for orbital insertion.

Design and Construction

Standing approximately 29.86 meters (98 feet) tall and measuring 2.25 meters (7 feet 5 inches) in diameter, the Long March 1 had a liftoff mass of about 81,570 kilograms (179,830 pounds). It was capable of delivering payloads up to 300 kilograms (660 pounds) into low Earth orbit (LEO).

The launch vehicle featured a three-stage configuration:

  • First Stage: Powered by a YF-2A engine, comprising four YF-1A engines, utilizing unsymmetrical dimethylhydrazine (UDMH) as fuel and AK27S (a nitric acid oxidizer) as the oxidizer.

  • Second Stage: Equipped with a YF-3A engine, also burning UDMH and AK27S.

  • Third Stage: Known as FG-02, this solid-propellant stage used a polysulfide and ammonium perchlorate (AP) mixture.

Mission Objectives

The Long March 1’s most notable mission occurred on April 24, 1970, when it successfully launched China’s first satellite, Dong Fang Hong 1, into orbit, making China the fifth nation to achieve independent satellite launch capability.

Launch and Deployment

The rocket had a brief operational period, with only two launches between 1970 and 1971, both of which were successful. Following these missions, it was retired in favor of more advanced launch vehicles in the Long March series.

Technical Specifications

  • Height: 29.86 meters (98 feet)
  • Diameter: 2.25 meters (7 feet 5 inches)
  • Mass: 81,570 kilograms (179,830 pounds) at liftoff
  • Payload Capacity: Up to 300 kilograms (660 pounds) to low Earth orbit (LEO)
  • Propellant Type: Liquid (UDMH as fuel and AK27S as oxidizer for first and second stages)
  • Stages: Three-stage configuration (First and second stages with liquid propellant, third stage for orbital insertion)

Current Status

The development and success of the Long March 1 marked a significant milestone in China’s space exploration efforts, laying the groundwork for the country’s subsequent advancements in launch vehicle technology.

More Spacecraft Propulsion

From traditional chemical rockets to innovative ion drives and beyond, propulsion systems propel spacecraft across vast distances, enabling exploration, scientific discovery, and satellite deployment. Explore more:

Virgin Space Ship Unity - Spacecraft & Space Vehicles Database

VSS Unity

Explore VSS Unity, Virgin Galactic’s revolutionary spacecraft offering suborbital spaceflight experiences and experience weightlessness.

Read More »
OmegA Rocket - Spacecraft Propulsion - Solid Fuel - USA

OmegA Rocket

Explore the OmegA rocket, Northrop Grumman’s heavy-lift launch vehicle designed for commercial and government missions.

Read More »
Juno I Rocket - Spacecraft Liquid Fuel Propulsion - United States

Juno I Rocket

Discover the historic significance of the Juno I rocket, the launch vehicle that propelled the United States into the space age.

Read More »