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Gateway To Space ASEN / ASTR 2500 Class #19. T-18. Colorado Space Grant Consortium. One minute:. Today:. Announcements One Minute Reports Mid semester Team Evaluation Due Camera Programming Questions Rest of Launch Vehicles
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Gateway To Space ASEN / ASTR 2500 Class #19 T-18 Colorado Space Grant Consortium
Today: • Announcements • One Minute Reports • Mid semester Team Evaluation Due • Camera Programming Questions • Rest of Launch Vehicles • Next Classes – Spider (Thur) and Pre-launch inspection (Tues) -> Bring your hardware
Announcements - Project help at Space Grant - Most people will help if you schedule a time to get that help - Use Tim May - Hardware? - My next four weeks…
Announcements - My next four weeks…
Announcements - My next four weeks…
Announcements - My next four weeks…
Announcements - My next four weeks…
Announcements - My next four weeks…
Announcements - My next four weeks…
Announcements - My next four weeks…
Announcements - My next four weeks…
One Minute Reports: - What launch vehicle took the Mars Rover to Mars? - Why was China putting that guy in space more important than the X-prize? - What other countries have real serious space programs? - Sea Launch – Private or government? - Cost/kg lower because of Russia/China labor costs? - What is your favorite old rocket? - What made the Saturn V carry so much cargo? - What are some of the reasons rockets blew up? - Do you think Saturn V was a better a launch vehicle to transport humans?
One Minute Reports: - What launch vehicle took the Mars Rover to Mars? - Why was China putting that guy in space more important than the X-prize? - What other countries have real serious space programs? - Sea Launch – Private or government? - Cost/kg lower because of Russia/China labor costs? - What is your favorite old rocket? - What made the Saturn V carry so much cargo? - What are some of the reasons rockets blew up? - Do you think Saturn V was a better a launch vehicle to transport humans?
One Minute Reports: - Why didn’t they pass down the knowledge for the Saturn V? - Which country is the US most likely to work with in the future (space-wise)? - What direction do you think we should take (Augustine report)? - Should we watch the Right Stuff? - Don’t the engineer know that they don’t have enough thrust? - Space elevator replace rockets? - Where do you get to eat under a Saturn V?
One Minute Reports: - Why didn’t they pass down the knowledge for the Saturn V? - Which country is the US most likely to work with in the future (space-wise)? - What direction do you think we should take (Augustine report)? - Should we watch the Right Stuff? - Don’t the engineer know that they don’t have enough thrust? - Space elevator replace rockets? - Where do you get to eat under a Saturn V?
One Minute Reports: - What do we have to have done for preflight inspection? - Can we watch the movie “The Right Stuff?” - If camera stops working, who do we talk to? - How far should we be through our project at this point? - Camera display date and time on picture? - These cameras are evil! - Can we get more hot glue for free? - Why do we use aluminum tape instead of duck tape?
One Minute Reports: - Will we see the results of the team evaluations? - What is the temperature of outer space? - Does our whole group get the same grade? - Will space propulsion be on the test? - What are the three sheets of foam core?
One Minute Reports: - Will we see the results of the team evaluations? - What is the temperature of outer space? - Does our whole group get the same grade? - Will space propulsion be on the test? - What are the three sheets of foam core?
Launch Vehicles Part 2 Class #18 Colorado Space Grant Consortium
Present: • Foreign • France (Ariane) • Japan (H-series) • China (Long March) • Russia (Proton, Buran) • United States • Shuttle • Atlas • Titan • Delta • Pegasus • Athena • Taurus • Falcon • ARES • Dragon (COTS) • Orion
Present: Space Shuttle Thrust: 28,200,000 N (6,340,000 lb) Fueled Weight: 2,040,000 kg Payload to Orbit: 24,400 kg LEO Cost per launch: $245,000,000 Cost per kg: $10,040 SRB Recovery External Tank
Present: First Shuttle Flight Video
Present: SRB Separation Video
Present: External Tank Video
Present: Atlas IIAS Thrust: 2,980,000 N (670,000 lb) Fueled Weight: 234,000 kg Payload to Orbit: 8,390 kg LEO Cost per launch: $78,000,000 Cost per kg: $9,296
Present: Atlas II Video
Present: Titan IV Thrust: 4,800,000 N (1,080,000 lb) Fueled Weight: 860,000 kg Payload to Orbit: 21,645 kg LEO Cost per launch: $248,000,000 Cost per kg: $11,457
Present: Titan IV Video
Present: Delta II Thrust: 2,630,000 N (591,000 lb) Fueled Weight: 230,000 kg Payload to Orbit: 5045 kg LEO 17,000 kg Cost per launch: $60,000,000 Cost per kg: $11,892
Present: Delta IV Height 63 - 77.2 m (206 - 253.2 ft) Diameter 5 m (16.4 ft) Mass 249,500 - 733,400 kg (550,000 - 1,616,800 lb) Stages 2 Capacity Payload to LEO 8,600 - 25,800 kg (18,900 - 56,800 lb) Payload to GTO
Present: Pegasus Thrust: 486,000 N (109,000 lb) Fueled Weight: 24,000 kg Payload to Orbit: 455 kg LEO Cost per launch: $9,000,000 Cost per kg: $19,800
Present: Pegasus Video
Present: Ariane 44L (France) Thrust: 5,380,000 N (1,210,000 lb) Fueled Weight: 470,000 kg Payload to Orbit: 9,600 kg LEO Cost per launch: $110,000,000 Cost per kg: $11,458
Present: Ariane 5 (France) Thrust: 11,400,000 N (2,560,000 lb) Fueled Weight: 737,000 kg Payload to Orbit: 18,000 kg LEO Cost per launch: $120,000,000 Cost per kg: $6,666
Present: Ariane V Video
Present: H-2 (Japan) Thrust: 3,959,200 N (890,060 lb) Fueled Weight: 260,000 kg Payload to Orbit: 10,500 kg LEO Cost per launch: $190,000,000 Cost per kg: $18,095 Video
Present: H2 Video
Present: Long March CZ2E (China) Thrust: 5,922,000 N (1,331,000 lb) Fueled Weight: 464,000 kg Payload to Orbit: 8,800 kg LEO Cost per launch: $50,000,000 Cost per kg: $5,681
Present: Sea Launch / Zenit Widest Diameter: 14 feet Overall length: Approximately 200 feet All stages are kerosene/liquid oxygen fueled Capacity to geosynchronus transfer orbit: 6,000 kg
Present: Proton D-1 (Russia) Thrust: 9,000,000 N (2,000,000 lb) Fueled Weight: 689,000 kg Payload to Orbit: 20,000 kg LEO Cost per launch: $70,000,000 Cost per kg: $3,500