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Space Launch System

Space Launch System

Space Launch Systems
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Basic Information
Name
Space Launch System
Designation
Space Launch System
Alternate Designation
Equipment Type
Space Launch Systems
Manufacturer
Date of Introduction
Description

The NASA's Space Launch System (SLS) is a deep space exploration initiative aimed at developing a family of modular heavy-lift launch vehicles to transport spaceships and equipment. The SLS program has been designed to replace the failed Ares I and Ares V space rockets while delivering a more affordable and sustainable launch vehicles. The SLS rocket will incorporate technological investments from the Space Shuttle Program and the Constellation Program in order to take advantage of proven hardware and cutting-edge tooling and manufacturing technology that will significantly reduce development and operations costs. The core stage utilizes three to five RS-25D/E rocket engines that burns a mixture of liquid hydrogen and liquid oxygen. The J-2X rocket engine using liquid hydrogen and liquid oxygen has been selected for the upper stage. Besides, SLS will also use solid rocket boosters and follow-on boosters based on performance requirements. The first development flight is targeted for the end of 2017. The new exploration-class vehicle since the Saturn V that took the United States of America to the Moon should be operational by 2018. SLS should expand NASA's reach in the solar system and allow to explore the space around the Moon, near-Earth asteroids, Mars and its moons and beyond. Its modular architecture is aimed to configure each launch vehicle for specific mission needs using a variation of common elements to achieve a variety of payload volumes and weights.

Overview (Deagel)
Group Space Launch Systems
Status Active
Also Known As SLS Block 1, SLS Block 1B
Origin United States of America
Contractors Aerojet Rocketdyne, Boeing, Northrop Grumman, United Launch Alliance
Initial Operational Capability (IOC) April 1, 2026
First Flight November 16, 2022
Total Production 5
Development Cost USD $41 billion
Unitary Cost USD $3 billion
Specifications (Deagel)
Number of Stages 1
Dimensions — Height 98 meter
Dimensions — Rocket Diameter 8.4 meter
Mass — Max Lift-off Thrust 39,100 kN
Mass — Max Lift-off Weight 2,495 ton
Mass — Payload to LEO 105 ton
Mass — Payload to Moon 38 ton
Volume — Payload Capacity 70 metric ton
Gear (Deagel)
Item 1 Rocket Engines: RS-25D/E (5)
Item 2 Rocket Engines: Solid Rocket Booster (2)
Item 3 Spaceships: Orion (1)
Variants
Variant 1 SLS Initial Lift Capability
Variant 2 SLS Evolved Lift Capability
Details
Country of Origin United States
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
98 m
Width
8.4 m
Height
98 m
Weight
2495000 kg
Operators (1)
United States
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