Ultra Large Solar Sail Technology

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$499,938.00
Award Year:
2004
Program:
STTR
Phase:
Phase II
Contract:
NNM04AB18C
Agency Tracking Number:
020025
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
CU Aerospace LLC
60 Hazelwood Dr., Champaign, IL, 61820
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
041929402
Principal Investigator:
David Carroll
Principal Investigator
() -
carroll@cuaerospace.com
Business Contact:
David Carroll
Business Official
(217) 333-8274
carroll@cuaerospace.com
Research Institution:
University of Illinois, U-C
Paul W Bohn
306 Talbot Lab/104 S. Wright St.
Urbana, IL, 61801
(217) 333-0678
Nonprofit college or university
Abstract
UltraSail, proposed by a team of CU Aerospace, the University of Illinois at Urbana-Champaign, SRS Technologies, and VACCO Industries, is a next-generation high-risk, high-payoff sail system for the launch, deployment, stabilization and control of very large (km^2 class) solar sails enabling high payload mass fractions for interplanetary and deep space spacecraft. UltraSail is an innovative, non-traditional approach to propulsion technology achieved by combining propulsion and control systems developed for formation-flying microsatellites with an innovative solar sail architecture to achieve controllable sail areas approaching 1 km^2, sail subsystem area densities approaching 1 g/m^2, and thrust levels many times those of ion thrusters used for comparable deep space missions. UltraSail can achieve outer planetary rendezvous, a deep space capability now reserved for high-mass nuclear and chemical systems. The primary innovation presented in Phase I was the near-elimination of sail supporting structures by attaching each blade tip to a formation-flying microsatellite which deploys the sail, and then articulates the sail to provide attitude control, including spin stabilization and precession of the spin axis. These tip microsatellites are controlled by a 3-axis microthruster metrology system to control sail film deployment.

* information listed above is at the time of submission.

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