STS's mains characteristics
Characteristic | Value |
Mass of STS at the beginning, t | 2046 |
Thrust at launch, tf | 3076 |
Specification of the Orbiter | |
Mass at launch, t | 109 |
Maximum mass at landing, t | 96 |
Payload mass, t | 20 |
Volume of the crew cabine, m³ | 71 |
Dimensional specifications | |
Length, m | 34.24 |
Wingspan, m | 23.79 |
Height, m | 17.25 |
Length of the payload bay, m | 18.3 |
Diameter of the payload bay, m | 4.6 |
Quantity of flight | 100 |
Mass of the structure, t | 68.586 |
Heat shield tiles, number | 24000 |
Circular work orbit, km | 185 to 1000 |
Crew | 7 |
Total mass of the 1st stage, t | 1180 |
Mass of solid fuel, t | 950 |
Pulverulent aluminium powder (combustible), % | 16 |
Perchlorate of ammonium (combustive), % | 69.6 |
Iron oxyde powder (catalyst), % | 0.4 |
Polybutadiene Acrylonitrile or Hydroxyl-terminated polybutadiene (polymer), % | 12 |
Epoxy curring agent (catalyst), % | 2 |
Total mass of the 2nd stage, t | 757 |
Mass of oxygen, t | ~600 |
Mass of hydrogen, t | ~100 |
Engine of the 2nd stage (SSME) | |
Thrust on the sea level (100% thrust), tf | 170 |
Thrust in vacuum (100% thrust), tf | 213 |
Dimensional specifications of the STS | |
Height, m | 56.14 |
Width, m | 23.79 |
Dimensional specifications of the 1st stage | |
Height, m | 45.6 |
Diameter, m | 3.71 |
Dimensional specifications of the external tank | |
Height, m | 46.9 |
Diameter, m | 8.4 |
Uses | |
1st stage, flight | 20 |
2nd stage (external tank), flight | 100 (1) |
Azimuth of launch, ° | 35-120 |
Minimal duration between 2 consecutive flights, days | 25 |
The former Soviet Union's analogue was the Energiya-Buran launch The decision to go forward with development of system was made in 1974-1976 but the program slow to gear up. The Buran (snowstorm or orbiter was not launched atop the Energiya launch until 1988, although an Energiya test launch was successfully without the Buran in 1987. During the test flight, Buran flew two orbits without a and successfully returned to Earth. This turned out be the Buran's one and only flight. The was put on hold and then cancelled in
Beyond appearances, however, there are several important technical differences the two Shuttle systems. Perhaps the most significant that the U.S. Shuttle was always intended to people into space but on its only flight, Buran flew without a crew, although it was to accommodate human crews as well. At one clearly the U.S. Shuttle was designed as a program to the Apollo and Skylab projects that send humans aloft on a routine basis. As Wolfe described in The Right Stuff, the U.S. NASA aerospace cultures were dominated first by pilots then by astronauts, so some might say that people, not just payloads, into space was always priority. This is still true today, as NASA's spaceflight efforts on Shuttle and the International Space spark the public's imagination and pave the way and budgetarily for robotic spacecraft missions, ground-based astronomy, even aeronautics.