There are 2 images added on 11 October 2018
Initial Operational Capability (IOC):
Origin: United States of America
Parent System: OmegA
Initial Operational Capability (IOC): 2022
Maiden Flight: 2021
Total Production: ?
Development Cost: USD$792 million
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Description: The OmegA is a family of space launch systems developed by Northrop Grumman to meet the requirements of the US Air Force (USAF) Evolved Expandable Launch Vehicle (EELV) program. The OmegA family includes intermediate and heavy variants which are slated for launch in 2021 and 2024 respectively. The intermediate variant will be ready to conduct commercial and military launches in 2022. The rocket configuration features first and second stages powered by CASTOR engines utilizing solid propellant with strap-on boosters. The upper stage is powered by an RL-10C liquid propellant engine. In October 2018 the USAF awarded Northrop Grumman a $792 million for the OmegA rocket family which is aimed at both civilian and military customers.
Number of Stages: 3
Payload to GTO: 10,100 kilogram (22,266 pound)
CEP: Circular Error Probable
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
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10 Oct 2018 and 10 Oct 2018
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