LEADER 01717cam  22004217a 4500001    ocm42019955
003    OCoLC
005    20141212132751.0
008    990805s1999    ohu     b    f000 0 eng d
035    (Sirsi) o42019955
035    (OCoLC)42019955
040    GPO |cGPO |dDLC |dMvI |dUtOrBLW
049    ERE$
074    0830-D (MF)
086 0  NAS 1.15:208906
245 04 The Microgravity Isolation Mount : |ba linearized state-space model á la Newton and Kane / |cR. David Hampton [and others].
246 30 Linearized state-space model a la Newton and Kane
260    [Cleveland, Ohio] : |bNational Aeronautics and Space Administration, Lewis Research Center ;[Springfield, Va.] : |b[National Technical Information Service, distributor], |c[1999]
300    1 volume.
336    text |2rdacontent
337    microform |2rdamedia
338    microfiche |2rdacarrier
490 1  NASA/TM ; |v1999-208906
500    Shipping list no.: 99-0703-M.
533     |3Joyner-Microfiche. |b[Washington, D.C. : |cNational Aeronautics and Space Administration, |d1999] |e1 microfiche.
650  7 Vibration isolators. |2nasat
650  7 Mathematical models. |2nasat
650  7 Vibration damping. |2nasat
650  7 Structural design. |2nasat
650  7 Controllers. |2nasat
650  7 Structural dynamics. |2nasat
650  7 Spacecraft components. |2nasat
700 1  Hampton, R. David. |?UNAUTHORIZED
710 2  Lewis Research Center. |=^A367825
830  0 NASA technical memorandum |v208906. |=^A467613
596    1
998    660787