Trailblazer 2
In-active TrailblazerNational Aeronautics and Space Administration (NASA)
Dec. 14, 1961
Description
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
Government
Administrator: Bill Nelson
NASA 1958The 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.
Trailblazer 2 | Trailblazer Pellet
National Aeronautics and Space Administration | USAWallops Island, Virginia, USA
Feb. 14, 1967, 5:52 a.m.
Trailblazer 2 | Trailblazer Pellet
National Aeronautics and Space Administration | USAWallops Island, Virginia, USA
March 18, 1966, 1:15 a.m.
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