Trailblazer Pellet

Overview

Destination: Suborbital
Mission: Materials Science

Suborbital Unknown Pad Wallops Island, Virginia, USA

Suborbital launch to test re-entry systems. Reached an apogee of 280 km.

Trailblazer 2

Family: Trailblazer
Configuration: 2

American test vehicle. NASA rocket designed for high-speed re-entry tests.

Specifications
  • Stages
    4
  • Length
    15.7 m
  • Diameter
    0.79 m
  • Fairing Diameter
    0.79 m
  • Launch Mass
    6 T
  • Thrust
    547 kN
Family
  • Name
    Trailblazer 2
  • Family
    Trailblazer
  • Variant
    2
  • Alias
  • Full Name
    Trailblazer 2
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

National Aeronautics and Space Administration

Circle Image
Administrator: Bill Nelson Founded: 1958 Successes: 114 Failures: 20 Pending: 6

Agency Type: Government

The National Aeronautics and Space Administration is an independent agency of the executive branch of the United States federal government responsible for the civilian space program, as well as aeronautics and aerospace research. NASA have many launch facilities but most are inactive. The most commonly used pad will be LC-39B at Kennedy Space Center in Florida.

INFO WIKI

Wallops Island, Virginia, USA

Unknown Pad


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