home *** CD-ROM | disk | FTP | other *** search
/ Chip 1997 October / Chip_1997-10_cd.bin / oddech / expedice / 11delta.gif < prev    next >
Graphics Interchange Format  |  1997-08-19  |  60KB  |  630x420  |  8-bit (241 colors)
Labels: airplane | bulletin board | monitor | sky | sounding board | space helmet | stairs | tree
OCR: Mars Global Surveyor Project Delta JPL Launch Vehicle Launch Vehicle McDonnell Douglas Aerospace Delta 7925 Overall Length: 38.2 m Core Diameter: First Stage: Main Engine: Rocketdyne RS-27 with 894 kN of thrust Propellant: 96 000 kg of RP-1 fuel and liquid oxygen Augmentation Solid Rockets: Nine 440 kN thrust solid- -propellant graphite epoxy motors Propellant 12,000 kg each of hydroxyl- terminated polybutadlene Second Stage: Engine: Aerojet AJ10-118K with 42 kN of thrust Propellant: 6000 ke of Aerozine 50 fuel and nitrogen tetroxide Third Stage Engine: Star-48B solid rockei motor with 67 kN thrust Propellant: ,000 ka of ammonium perchlorate and aluminum Spin Table to support rotate and stabilize the upper stage Survevor NASA rocket