Table Manned Apollo Missions
First manned flight test of the command service module First manned test flight of the Apollo Saturn vehicle in lunar orbit To test lunar landing hardware while in earth orbit To test lunar landing hardware while in lunar orbit To undertake the first manned lunar landing Second lunar landing Perform surface experiments Investgigate the remains of Surveyor III Third lunar landing Perform surface experiments Fourth lunar landing Use lunar rover vehicle Fifth Lunar landing Exploration of the...
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PROJECT GEMINI BIBLIOGRAPHY 1962-1967 UTTl NASA-INDUSTRY Apollo Technical Conference, part 2 COUP National Aeronaut Ics anil Space Administration. Washington. 0. C. 69N71684 RPT NASA TM-X-50045 61 07 20 UT1L Electric power supply system for Apollo AUTH A ALI TN, G. 0. B COLEHOWER. E. W. C SCALES. S. H. CORP Martin Co Baltimore. Md. 69N7I6I9 61 07 20 UTTL Im atm electrical power system AUTH A MOSS. B. W. CORP Be IIcomm. Inc Washington. D. C. 79N72 lt 45 RP T NASA-CR-93015 CNT NASW-417 67 12 20...
Apollo Program
The first Apollo mission launch date was October 27, 1961 and it verified the Saturn I's aerodynamic and structural design. A series of five more launches were conducted before the first manned Apollo launch was made on October 11, 1968. See Table 4.1 for details of Apollo missions 1 . On July 16, 1969, man landed on the moon Apollo 11 mission followed by five more moon landings. The last launch was on December 7, 1972. See Table I for The Apollo command and service module electrical power...
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UTTL Voyager capsule phase 8. Volume III - Surface laboratory system. Part CI - Subsystem functional descr ipt Ion Final report UNOC Voyager capsule surface laboratory system - subsystem functional descriptions CORP Jet Propulsion Lab California lot.I. of Tech., Pasaoena. McDonnell Aircraft Co., St. Louis, Mo. 67N40585 RPT NASA-CR-89695 F694, VOL. III. PT. CI CNT NAS7-I00 JPL-952000 67 08 31 VOYAGER MISSION BIBLIOGRAPHY 1962-1967 PR I Nf 23 4 1 -20 T ERMI NALS 73 UTIL Electrical power system...
Project Gemini
Experience from Project Mercury demonstrated that failure propagation can occur when the systems are designed such that there is an interdependency or when systems are installed in a stacked fashion with common interfaces. In order to remove this constraint, Gemini development program emphasized rigorous . Component Testing . Subsystem Testing . Integrated Systems Testing The Gemini systems were almost exclusively installed In a modular structure outside the inner pressure vessel and were...
Viking Project
The principle objective of the Viking Project was to send two vehicles, each consisting of an Orbiter System and a Lander System, to Mars to perform scientific experiments to enlarge our present knowledge about the physical characteristics of Mars, especially its ability for supporting life 1 . Viking 1 and 2 were launched in August and September, 1975, respectively. The design of the Viking Orbiter was essentially based on the Mariner spacecraft series. The design philosophy was to scale-up...
Project Mercury Bibliography
UTIL Proceedings of a conference on results of the first u.s. manned suborbital space flight AUTH A DRYDEN. H. I. CORP NE36B37J 64N8045B RPT NASA-TM-X-SI3B0 61 06 06 UNOC Results of the second u.s. manned orbital space flight, may 24. 1962 CORP N0300209 62N14691 R P T NASA-SP-6 62 00 00 UNOC Spacecraft and Iaunch-vehIcIe performance, mission operations, aeromedlcal analysis, pilot performance, pilots flight report CORP ND380289 63N11990 RPT NASA-SP-12 62 10 03
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UIrI Mercury manned orbital capsulo detall sp cl Meat ion AUTM A PARKER. I. M. CORP McDonnell Aircraft Co., St. Louis. Mo. 75N76020 RP f NASA-CR-55594 REPT-6603 CNT r NAS5- 59 60 00 25 UlTL Mercury capsule no. 14. configuration s-pecl Meat Ion Mercury - LI 11 le -toe No. 5 A AUTH A koi.ANDO. R. D. CORP McDonnell Aircraft Co St. Louis. Mo. 74N7I549 RPT NASA-CR-50068 RE PT - fj603 - I 4 CNT NAS5-59 61 01 20 UTIL Project Mercury Technical Information summary of Mercury-Redstone mission no. 3....
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Dill Space Shuttle Orblter electrical power requirements. UNOC Space shuttle orblter electrical power system requirements and constraints, considering hydrogen oxygen fuel cell for compact energy storage imd turbine driven generators AUTH A SOllO, C. PAA A McDonnell Douglas Astronautics Co St. touts, Mo. 73A22776 72 00 00 UTTl Space Shuttle AUTH A ANDREWS, E. P. PAA A NASA. Space Shuttle Program OffIce, Washington. D.C. 75A19436 74 00 00 UTTL Shuttle Electrical Power Analysis Program SEPAP...
Skylab
SPACE SHUTTLE PROGRAM 6,1 PIONEER MISSION 8,1 MARINER RANGER PROJECT 10 '1 LUNAR ORBITER SURVEYOR PROJECT 12,1 VIKING PROJECT 13,1 VOYAGER CONCLUDING REMARKS 16,1 BIBLIOGRAPHY 17,1