| Record ID | marc_oregon_summit_records/catalog_files/washs02192008.mrc_revrev.mrc:65094410:1174 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/washs02192008.mrc_revrev.mrc:65094410:1174?format=raw |
LEADER: 01174nam a22003131a 4500
001 22303236
008 900831r19881988dcu b f000 0 eng d
027 $aE-4204
035 $a(GPO)90021286
040 $aGPO$cGPO$dMvI
049 $aNTEI
074 $a830-D (MF)
086 0 $aNAS 1.15:100933
100 1 $aQuentmeyer, Richard J.
245 10 $aThrust chamber thermal barrier coating techniques$h[microform] /$cRichard J. Quentmeyer.
260 0 $a[Washington, DC] :$bNational Aeronautics and Space Administration ;$a[Springfield, Va. :$bFor sale by the National Technical Information Service,$c1988]
300 $a1 v.
440 0 $aNASA technical memorandum ;$v100933.
533 $aMicrofiche.$b[Washington, D.C.? :$cNational Aeronautics and Space Administration],$d1988.$e1 microfiche.
500 $aDistributed to depository libraries in microfiche.
650 0 $aRocket engines.
650 0 $aCeramic coating.
710 1 $aUnited States.$bNational Aeronautics and Space Administration.
907 $a.b11954462$bwo $c-
902 $a070724
998 $b1$c980919$dm$ea$f-$g0
907 $a.b11954462
907 $a.b11954462
945 $lwoxau$aNAS 1.15:100933