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Project Antares: A low cost modular launch vehicle for the futureThe single stage to orbit launch vehicle Antares is based upon the revolutionary concept of modularity, enabling the Antares to efficiently launch communications satellites, as well as heavy payloads, into Earth's orbit and beyond. The basic unit of the modular system, a single Antares vehicle, is aimed at launching approximately 10,000 kg into low Earth orbit (LEO). When coupled with a Centaur upper stage it is capable of placing 3500 kg into geostationary orbit. The Antares incorporates a reusable engine, the Dual Mixture Ratio Engine (DMRE), as its propulsive device. This enables Antares to compete and excel in the satellite launch market by dramatically reducing launch costs. Antares' projected launch costs are $1340 per kg to LEO which offers a tremendous savings over launch vehicles available today. Inherent in the design is the capability to attach several of these vehicles together to provide heavy lift capability. Any number of these vehicles, up to seven, can be attached depending on the payload and mission requirements. With a seven vehicle configuration Antares's modular concept provides a heavy lift capability of approximately 70,000 kg to LEO. This expandability allows for a wider range of payload options such as large Earth satellites, Space Station Freedom support, and interplanetary spacecraft, and also offers a significant cost savings over a mixed fleet based on different launch vehicles.
Document ID
19920011425
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Aarnio, Steve
(Washington Univ. Seattle, WA, United States)
Anderson, Hobie
(Washington Univ. Seattle, WA, United States)
Arzaz, El Mehdi
(Washington Univ. Seattle, WA, United States)
Bailey, Michelle
(Washington Univ. Seattle, WA, United States)
Beeghly, Jeff
(Washington Univ. Seattle, WA, United States)
Cartwright, Curt
(Washington Univ. Seattle, WA, United States)
Chau, William
(Washington Univ. Seattle, WA, United States)
Dawdy, Andrew
(Washington Univ. Seattle, WA, United States)
Detert, Bruce
(Washington Univ. Seattle, WA, United States)
Ervin, Miles
(Washington Univ. Seattle, WA, United States)
Date Acquired
September 6, 2013
Publication Date
June 14, 1991
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NAS 1.26:190018
NASA-CR-190018
Accession Number
92N20667
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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