![](https://ci6.googleusercontent.com/proxy/xCaeHJpSXiigI4nn6UInMWlyzh6PdLHm5tSUluau7WFW8Jt8bUaVlYTl7mYYu-aRV3jFsEB_hnHXwutMNpPgr55u13ClHVAa0M1OhPvq7yGv5vzs576YED9ICJjVngEkkvpReYvxcmi8guPsHkyLsii1BCgGdxy5Kw=s0-d-e1-ft#https://jayabarathan.files.wordpress.com/2017/12/first-falcom-heavy-rocket-launch-testing.jpg?w=584)
![Image result for Behold! SpaceX's 1st Falcon Heavy Rocket on the Launchpad](https://ci5.googleusercontent.com/proxy/8LF4JzWYEhjOnbYufY9t4BlmyHuerNltozc3V83a7aVl2Pa0noHqpOGfSAxvKBn76g09AScO2un1q9AuVqAJ9LCoz3HxsZFxY7INDwYjd_dnWhrfZdSZ7r46LCpWxMtFC1vBk9Hdb940HaQcEWm4M8iD38GqQtoFwFtWgdxfspWf8g=s0-d-e1-ft#https://i0.wp.com/i.dailymail.co.uk/i/pix/2015/12/14/21/2F60218E00000578-3359967-image-a-1_1450130304220.jpg)
![]() The Tesla Roadster mounted on its payload adapter before fairing encapsulation
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OPERATOR | SpaceX |
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MANUFACTURER | Tesla |
INSTRUMENT TYPE | Inert mass |
FUNCTION | Dummy payload |
WEBSITE | spacex.com |
PROPERTIES | |
MASS | Approximately 1,300 kg (2,900 lb) |
HOST SPACECRAFT | |
LAUNCH DATE | January 2018 |
ROCKET | Falcon Heavy |
LAUNCH SITE | Kennedy LC-39A |
ORBIT | Heliocentric |
![](https://ci5.googleusercontent.com/proxy/pftkDtyK13fWmOSDFBQNPaK85NZP74I0xDISdgI-rTDuJzaNK6a7KvpFoM0eRAurCmcPkenzL8EK1Zw9_jH3I2KqNf72dTUKaBz4cArd6qCSzNGmHwEm5U9QNupew9RvO-Wpqf5qevfvBW5xlnRIvhgF1vS1PxnRe5ZA8DGUiCScCtAKcicV_L2eCH5dOBpE=s0-d-e1-ft#https://i1.wp.com/www.spacex.com/sites/spacex/files/styles/featured_news_widget_image/public/field/image/dragoncrew.8k.jpg)
![SpaceX Pad Abort Test Infographic](https://ci3.googleusercontent.com/proxy/dxlzJWVVlrrFWeJ7MDYqNXyl6G2kjw4wi8KzsnGb7ZGLvHYPAK9aHJ5voqO1mIQALTD-0IbEQ3JTyoYRKVOxESLP4LmyUB5DAkOaDIU_42bJVsWPYWwy9o4YVSXFHPYtbA=s0-d-e1-ft#https://i2.wp.com/www.spacex.com/sites/spacex/files/padabortinfographic.jpg)
![A close-up of Musk's face while giving a talk](https://ci4.googleusercontent.com/proxy/Wb1zPwHJco10yGjTyIu_mZTMnvbSXIWp8U3hZptw6T23RrMyPNnlgnHvUmUo18o4qZKs6r9QdBHgjrjoRiwgihoK37whfk5gjidMWBxGTfaPrQfzEehDDHhdv7wIWQdA3uZYpVkJuBugdGIQPF8-W11rd8U6EK9WqCIa=s0-d-e1-ft#https://upload.wikimedia.org/wikipedia/commons/thumb/4/49/Elon_Musk_2015.jpg/220px-Elon_Musk_2015.jpg)
BORN | Elon Reeve Musk June 28, 1971 Pretoria, Transvaal (now Gaute |
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RESIDENCE | Bel Air, Los Angeles, California, U.S.[1][2] |
CITIZENSHIP |
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ALMA MATER | |
OCCUPATION | Entrepreneur, engineer, invent |
KNOWN FOR | SpaceX, PayPal, Tesla Inc., Hyperloop, SolarCity, Op |
NET WORTH | US$20.8 billion (October 9, 2017)[6] |
TITLE |
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SPOUSE(S) |
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CHILDREN | 6 |
PARENT(S) |
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RELATIVES |
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SIGNATURE | |
![]() |
![Image result for spacex heavy lift rocket](https://ci6.googleusercontent.com/proxy/Q9bgFdRSO2hl_Beh0p-ZTkIfBsGL1PJMqDoMUgugESvxtvP-MU6V63bKBNh0l_PG5t8v0N71SNIEhN5bc6c2RdEe4AUa3k1krHVhzGXpjFNo1GwvQ41BuChL0dOV5Hze=s0-d-e1-ft#https://i2.wp.com/www.wired.com/images_blogs/autopia/2011/04/callouts2.jpg)
![Image result for spacex heavy lift rocket](https://ci5.googleusercontent.com/proxy/TpiQwQBlDxFMQxIb9ODToeg4rypD4CrKbxL1-9kBszqPOhM3vu2AMW03NErgE_MkTr7K8GkASh_W269XmrKm3juXKON_BUXSNGoz5nbTrm4Q6S4n4WHnJxlw1izjXT9YHhHFWZ6M18Gp76rdviAVd6rwk0sIHw=s0-d-e1-ft#https://wordlesstech.com/wp-content/uploads/2015/01/The-ingenious-future-of-SpaceX-rockets-1.jpg)
![]() Falcon Heavy getting ready for its first launch
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FUNCTION | Orbital super heavy-lift launch vehicle |
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MANUFACTURER | SpaceX |
COUNTRY OF ORIGIN | United States |
COST PER LAUNCH | $90M for up to 8,000 kg to GTO[1] |
SIZE | |
HEIGHT | 70 m (230 ft)[2] |
DIAMETER | 3.66 m (12.0 ft)[2] |
WIDTH | 12.2 m (40 ft)[2] |
MASS | 1,420,788 kg (3,132,301 lb)[2] |
STAGES | 2+ |
CAPACITY | |
PAYLOAD TO LEO (28.5°) | 63,800 kg (140,700 lb)[2] |
PAYLOAD TO GTO (27°) | 26,700 kg (58,900 lb)[2] |
PAYLOAD TO MARS | 16,800 kg (37,000 lb)[2] |
PAYLOAD TO PLUTO | 3,500 kg (7,700 lb)[2] |
ASSOCIATED ROCKETS | |
FAMILY | Falcon 9 |
COMPARABLE | |
LAUNCH HISTORY | |
STATUS | on launchpad |
LAUNCH SITES | |
TOTAL LAUNCHES | 0 |
SUCCESSES | 0 |
FAILURES | 0 |
FIRST FLIGHT | January 2018 (planned)[3] |
BOOSTERS | |
NO. BOOSTERS | 2 |
ENGINES | 9 Merlin 1D |
THRUST | Sea level: 7,607 kN (1,710,000 lbf) Vacuum: 8,227 kN (1,850,000 lbf) |
SPECIFIC IMPULSE | Sea level: 282 seconds[4] Vacuum: 311 seconds[5] |
BURN TIME | 162 seconds[6] |
FUEL | Subcooled LOX / Chilled RP-1[7] |
FIRST STAGE | |
ENGINES | 9 Merlin 1D |
THRUST | Sea level: 22,819 kN (5,130,000 lbf) Vacuum: 24,681 kN (5,549,000 lbf)[2] |
SPECIFIC IMPULSE | Sea level: 282 seconds Vacuum: 311 seconds |
BURN TIME | 162 seconds |
FUEL | Subcooled LOX / Chilled RP-1 |
SECOND STAGE | |
ENGINES | 1 Merlin 1D Vacuum |
THRUST | 934 kN (210,000 lbf)[2] |
SPECIFIC IMPULSE | 348 seconds[6] |
BURN TIME | 397 seconds[2] |
FUEL | LOX / RP- |
60. https://www.space.com/3587
61. https://www.space.com/3766
62. https://en.wikipedia.org/w
63. https://en.wikipedia.org/w
64. https://futurism.com/falco
65. https://www.space.com/3926
66 https://en.wikipedia.org/wi
67. https://en.wikipedia.org/w
++++++++++++
S. Jayabarathan (jayabarathans@gmail.com) January 6, 2018 [R-4]
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