|
|
|
|
| LEADER |
03191nam a2200709Ka 4500 |
| 001 |
65c8e79a-fd61-4eba-a2b5-3e121b738170 |
| 005 |
20240728000000.0 |
| 008 |
050214s1984 ohu b f000 0 eng d |
| 019 |
|
|
|a 1031679430
|
| 035 |
|
|
|a (NcD)003421735DUK01
|
| 035 |
|
|
|a (OCoLC)57657241
|
| 035 |
|
|
|a (OCoLC-M)57657241
|
| 035 |
|
|
|a 1031785963
|
| 037 |
|
|
|a N 84-20699
|b NASA
|
| 040 |
|
|
|a GPO
|b eng
|c GPO
|d MvI
|
| 040 |
|
|
|a GPO
|b eng
|c GPO
|d OCLCQ
|d SYB
|d OCLCO
|d OCLCQ
|d OCLCO
|d OCLCQ
|d OCLCF
|d OCL
|d GPO
|d MvI
|
| 049 |
|
|
|c c1
|a STFD
|
| 074 |
|
|
|a 0830-H-14 (MF)
|
| 086 |
0 |
|
|a NAS 1.26:168321
|
| 088 |
|
|
|a BAC D 180-28274-1
|
| 092 |
|
|
|a x
|
| 099 |
|
|
|a NAS 1.26:168321
|
| 100 |
1 |
|
|a Kramer, T. J
|? UNAUTHORIZED
|
| 100 |
1 |
|
|a Kramer, T. J
|
| 245 |
1 |
0 |
|a Evaluation of propellant tank insulation concepts for low-thrust chemical propulsion systems :
|b executive summary /
|c by T.J. Kramer, E.W. Brogren, and B.L. Siegel
|
| 260 |
|
|
|a Cleveland, OH :
|b Lewis Research Center,
|c [1984]
|
| 264 |
|
1 |
|a Cleveland, OH :
|b Lewis Research Center,
|c [1984]
|
| 300 |
|
|
|a 1 v
|
| 300 |
|
|
|a 1 volume
|
| 336 |
|
|
|a text
|b txt
|2 rdacontent
|
| 337 |
|
|
|a microform
|b h
|2 rdamedia
|
| 338 |
|
|
|a microfiche
|b he
|2 rdacarrier
|
| 490 |
1 |
|
|a NASA CR ;
|v 168321
|
| 500 |
|
|
|a Distributed to depository libraries in microfiche
|
| 500 |
|
|
|a "BAC D180-28274-1."
|
| 500 |
|
|
|a "Boeing Aerospace Company."
|
| 500 |
|
|
|a "Contract NAS3-22824."
|
| 500 |
|
|
|a "Report date: March 1984"--Report documentation page
|
| 500 |
|
|
|a "Report date: March 1984"--Rept. documentation p
|
| 533 |
|
|
|a Microfiche
|b [Washington, D.C. :
|c National Aeronautics and Space Administration,
|d 1984].
|e 1 microfiche.
|
| 596 |
|
|
|a 1
|
| 650 |
|
0 |
|a Cryogenics
|? UNAUTHORIZED
|
| 650 |
|
0 |
|a Heat
|x Transmission
|
| 650 |
|
0 |
|a Space vehicles
|x Propulsion systems
|
| 650 |
|
7 |
|a Cryogenics
|2 nasat
|
| 650 |
|
7 |
|a Foam insulation
|2 nasat
|
| 650 |
|
7 |
|a Heat transfer
|2 nasat
|
| 650 |
|
7 |
|a Heat
|x Transmission
|2 fast
|
| 650 |
|
7 |
|a Space propulsion
|2 nasat
|
| 650 |
|
7 |
|a Space vehicles
|x Propulsion systems
|2 fast
|
| 650 |
|
7 |
|a Spacecraft propulsion
|2 nasat
|
| 700 |
1 |
|
|a Brogren, E. W
|? UNAUTHORIZED
|
| 700 |
1 |
|
|a Brogren, E. W
|
| 700 |
1 |
|
|a Siegel, B. L
|? UNAUTHORIZED
|
| 700 |
1 |
|
|a Siegel, B. L
|
| 710 |
2 |
|
|a Boeing Aerospace Company
|
| 710 |
2 |
|
|a Lewis Research Center
|
| 776 |
0 |
8 |
|i Online version:
|a Kramer, T.J
|t Evaluation of propellant tank insulation concepts for low-thrust chemical propulsion systems
|w (OCoLC)1038072568
|
| 830 |
|
0 |
|a NASA contractor report ;
|v NASA CR-168321
|
| 999 |
1 |
0 |
|i 65c8e79a-fd61-4eba-a2b5-3e121b738170
|l a5791700
|s US-CST
|m evaluation_of_propellant_tank_insulation_concepts_for_low_thrust_chemi_____1984_______lewisa________________________________________kramer__t__j_______________________nas_1_26_168321p
|
| 999 |
1 |
0 |
|i 65c8e79a-fd61-4eba-a2b5-3e121b738170
|l 990034217350108501
|s US-NCD
|m evaluation_of_propellant_tank_insulation_concepts_for_low_thrust_chemi_____1984_______lewisa________________________________________kramer__t__j_______________________nas_1_26_168321p
|
| 999 |
1 |
1 |
|l a5791700
|s ISIL:US-CST
|t BKS
|a GREEN FED-DOCS
|b 5791700-1001
|c NAS 1.26:168321
|d SUDOC
|x GOVSTKS
|y 5791700-1001
|p LOANABLE
|