Gat ew ay T o S pace AS EN / AS TR Class # 16. Colorado S pace Grant Consortium
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1 Gat ew ay T o S pace AS EN / AS TR 2500 Class # 16 Colorado S pace Grant Consortium
2 One Minute Paper: - Guest speaker not showing and letting us know - Checking out an extra HOBO? - What is a L-2 Orbit? - What happens if snowing on launch day? - When do we get reimbursed for our purchases? - Washers for flight string? - How far does temp probe have to extend from BalloonSat? - How Mars on saltwater? - Did we land on the moon for real? - How did Tskovisky know about the cradle? - Where do these rockets come in: Redstone, Atlas, Titan, Saturn - Why was Oberth so important? - How do you schedule cooler test? Do all electronics need to be inside?
3 One Minute Paper: - Order film? - Explain CoDR ranking? - How fast does BalloonSat hit the ground? - Condensation? -
4 CDR General Comments: - Most presentations improved from CoDR CDR in industry different than what you went through issues All parts ordered? We expect it to go fine or We don t expect any problems All payloads must be turned in ready to fly again and any problems understood and fixed - Take good pictures of payload inside and out before launch in case your payload never returns - Image/video tests are just as important as structural tests - Practice taking data off BalloonSat before flight
5 CDR General Comments: - Marv Luttges
6 CDR General Comments: Team Support from me Tuesday, October 24, 2006 please still come to class :00 9:15 9:15 9:30 9:30 9:45 9:45 10:00 10:00 10:15 10:15 10:30 10:30 10:45 10:45 11:00 11:45 12:00 1:00 1:15 Aquila Hubble Jr Cutthroat Wolverines Team 10 BioHazard Echo III Axium Justice Cobras
7 Announcements: - Movie Night Postponed - In Class time next Tuesday - Week from today Spacecraft Structures - Halloween will be special orbits lecture - Outreach form - Budget plan - 23 days until launch
8 Announcements:
9 Announcements:
10 Announcements:
11 Announcements:
12 Before we get started In Class Exercise
13 Building a Rocket on Paper: - Please wait, everyone will be opening your envelopes in a minute - Not every rocket design will work... - YOU ARE A ROCKET ENGINEER: You make $70, a year and you have a masters degree and drive a company Viper
14 Building a Rocket on Paper: 1.) Build a rocket with the right people. You will need Payload Specialist Thruster Specialist Fuel Expert Structural Engineer
15 Building a Rocket on Paper: 2.) Calculate total mass of your rocket, must include everything. Total mass = mass of fuel+payload+ structure+thrusters
16 Building a Rocket on Paper: 3.) Calculate the thrust needed to lift your rocket off the launch pad Needed thrust = total mass * gravity F = m * a [Newtons, N]) 1 N =1 kg*m/s2 1 pound-force = 4.45 N a=gravity=10 m/s2
17 Building a Rocket on Paper: 4.) Calculate the total lift (thrust) capability of your rockets thrusters 5.) Does your structure support the total weight of the rocket? 6.) Do you lift off the ground or did you crash and burn? 7.) Could you lift off the surface of the moon? g(moon) = 1/6 g(earth)
18 Ion Engine: Max Thrust = 200 N Engine/Fuel Mass = 9,000 kg (90,000 N) Max Thrust (minus Engine/Mass) = - 82,000 N Remaining Mass = - 8,200 kg Ashes (2 kg) Professor (180 kg) Stamps (2K kg) Water (20K kg) Tires (200K kg) Wood = 5K kg (200 kg) Composite = 9K kg (20 kg) Iron = 500K kg (20,000 kg) Aluminum = 3M kg (2,000 kg) Titanium = 5M kg (2,000 kg) Comments
19 Cold Gas Engine: Max Thrust = 22,000 N Engine/Fuel Mass = 1,700 kg (17,000 N) Max Thrust (minus Engine/Mass) = 5,000 N Remaining Mass = 500 kg Ashes (2 kg) Professor (180 kg) Stamps (2K kg) Water (20K kg) Tires (200K kg) Wood = 5K kg (200 kg) YES YES Composite = 9K kg (20 kg) YES YES Iron = 500K kg (20,000 kg) Aluminum = 3M kg (2,000 kg) Titanium = 5M kg (2,000 kg) Comments
20 Propane Engine: Max Thrust = 100,000 N Engine/Fuel Mass = 8,000 kg (80,000 N) Max Thrust (minus Engine/Mass) = 20,000 N Remaining Mass = 2,000 kg Ashes (2 kg) Professor (180 kg) Stamps (2K kg) Water (20K kg) Tires (200K kg) Comments Wood = 5K kg (200 kg) Structural Failure Composite = 9K kg (20 kg) YES YES Structural Failure Iron = 500K kg (20,000 kg) Aluminum = 3M kg (2,000 kg) Titanium = 5M kg (2,000 kg)
21 Liquid Engine: Max Thrust = 1,500,000 N Engine/Fuel Mass = 103,000 kg (1,030,000 N) Max Thrust (minus Engine/Mass) = 470,000 N Remaining Mass = 47,000 kg Ashes (2 kg) Professor (180 kg) Stamps (2K kg) Water (20K kg) Tires (200K kg) Comments Wood = 5K kg (200 kg) Structural Failure Composite = 9K kg (20 kg) Structural Failure Iron = 500K kg (20,000 kg) YES YES YES YES Aluminum = 3M kg (2,000 kg) YES YES YES YES Titanium = 5M kg (2,000 kg) YES YES YES YES
22 Solid Engine: Max Thrust = 3,000,000 N Engine/Fuel Mass = 52,000 kg (520,000 N) Max Thrust (minus Engine/Mass) = 2,480,000 N Remaining Mass = 248,000 kg Ashes (2 kg) Professor (180 kg) Stamps (2K kg) Water (20K kg) Tires (200K kg) Comments Wood = 5K kg (200 kg) Structural Failure Composite = 9K kg (20 kg) Structural Failure Iron = 500K kg (20,000 kg) YES YES YES YES Aluminum = 3M kg (2,000 kg) YES YES YES YES YES Titanium = 5M kg (2,000 kg) YES YES YES YES YES
23 Launch Vehicles Past, Present, Future & Sci-Fi Future
24 Outline: - Fine Print - Background & Rocket Types - Past - Present - Future - Sci-Fi Future
25 Rocket Types: - I don t know everything about Launch Vehicles - I may not be able to answer your questions - This lecture is to expose you to all the different types of launch vehicles - I can quit at any time
26 Background: - Thrust = the force that moves - Impulse = force over period of time - Specific Impulse = Isp = ratio of impulse to fuel used - Higher Isp usually indicates low thrust but very little fuel used - Will learn more in Propulsion Lecture - Rocket Types include: Solid, liquid, hybrid
27 Past
28 Past/Present: Scout Thrust: Fueled Weight: Payload to Orbit: 464,700 N (104,500 lb) 21,750 kg 270 kg LEO # of Flights: 188, 105 successful
29 Past: Jupiter C Thrust: Fueled Weight: Payload to Orbit: 334,000 N (75,090 lb) 29,030 kg 9 kg LEO (14 kg) # of Flights: 6, 4 successful Explorer I
30 Past: Mercury Redstone Thrust: Fueled Weight: Payload to Orbit: 347,000 N (78,000 lb) Not Found kg 9 kg LEO # of Flights: 5, 5 successful Chimp Ham, Shepard, and Grissom
31 Past: Mercury Redstone Video
32 Past: Go to the Moon Video
33 Past: Saturn V Thrust: Fueled Weight: Payload to Orbit: 34,500,000 N (7,760,000 lb) 2,910,000 kg 127,000 kg LEO
34 Past: The F1 Engine Video
35 Past:
36 Past: One Step Video
37 Past: Lunar Rover Video
38 Past: Apollo Astronaut Video
39 Saturn V: Can it be built today? Not really According to Prof. Jesco von Puttkamer, Program Manager of Future Planning at NASA in The blue prints still exist, however only on microfilm. - All the subcontractors and suppliers are no longer around. - The technology is old. We can build much smaller and lighter rockets today.
40 Present
41 Present: United States - Shuttle - Atlas - Titan - Delta - Pegasus - Athena - Taurus Foreign - France - Japan - China - Russia (Ariane) (H-series) (Long March) (Proton, Buran)
42 Present: Space Shuttle Thrust: Fueled Weight: Payload to Orbit: Cost per launch: Cost per kg: SRB Recovery External Tank 28,200,000 N (6,340,000 lb) 2,040,000 kg 24,400 kg LEO $245,000,000 $10,040
43 Present: First Shuttle Flight Video
44 Present: SRB Separation Video
45 Present: External Tank Video
46 Present: Atlas IIAS Thrust: Fueled Weight: Payload to Orbit: Cost per launch: Cost per kg: 2,980,000 N (670,000 lb) 234,000 kg 8,390 kg LEO $78,000,000 $9,296
47 Present: Atlas II Video
48 Present: Titan IV Thrust: Fueled Weight: Payload to Orbit: Cost per launch: Cost per kg: 4,800,000 N (1,080,000 lb) 860,000 kg 21,645 kg LEO $248,000,000 $11,457
49 Present: Titan IV Video
50 Present:
51 Present: Delta II Thrust: Fueled Weight: Payload to Orbit: Cost per launch: Cost per kg: 2,630,000 N (591,000 lb) 230,000 kg 5045 kg LEO 17,000 kg $60,000,000 $11,892
52 Present:
53 Present: Pegasus Thrust: Fueled Weight: Payload to Orbit: Cost per launch: Cost per kg: 486,000 N (109,000 lb) 24,000 kg 455 kg LEO $9,000,000 $19,800
54 Present:
55 Present: Pegasus Video
56 Present: Ariane 44L (France) Thrust: Fueled Weight: Payload to Orbit: Cost per launch: Cost per kg: 5,380,000 N (1,210,000 lb) 470,000 kg 9,600 kg LEO $110,000,000 $11,458
57 Present: Ariane 5 (France) Thrust: Fueled Weight: Payload to Orbit: Cost per launch: Cost per kg: 11,400,000 N (2,560,000 lb) 737,000 kg 18,000 kg LEO $120,000,000 $6,666
58 Present: Ariane V Video
59 Present: H-2 (Japan) Thrust: Fueled Weight: Payload to Orbit: Cost per launch: Cost per kg: Video 3,959,200 N (890,060 lb) 260,000 kg 10,500 kg LEO $190,000,000 $18,095
60 Present:
61 Present: H2 Video
62 Present: Long March CZ2E (China) Thrust: Fueled Weight: Payload to Orbit: Cost per launch: Cost per kg: 5,922,000 N (1,331,000 lb) 464,000 kg 8,800 kg LEO $50,000,000 $5,681
63 Yang Liwei
64 Present: Proton D-1 (Russia) Thrust: Fueled Weight: Payload to Orbit: Cost per launch: Cost per kg: 9,000,000 N (2,000,000 lb) 689,000 kg 20,000 kg LEO $70,000,000 $3,500
65 Present:
66 Present:
67 Present/Past: Energia (Russia) Thrust: Fueled Weight: Payload to Orbit: Cost per launch: Cost per kg: 34,800,000 N (7,820,000 lb) 2,400,000 kg 90,000 kg LEO $764,000,000? $Not Known
68 Present/Past: Buran Snowstorm (Russia) First and only launch November 15, 1988 No one on board - Life support not tested - CRT s did not have software Only 2 orbits - This was limited because of computer memory Landed by autopilot
69 Present/Past: Aero Buran was test unit Had 24 test flights 3 others were being built - Pitchka (Little Bird) - Baikal (Typhoon) All dismantled in 1995
70 Present/Past:
71 Present/Past:
72 Present/Past:
73 Present/Past:
74 Present/Past:
75 Present/Past:
76 Future
77 Future/Past:
78 Future/Past:
79 Future/Past:
80 Future/Past:
81 Future/Past:
82 Future/Past:
83 Future/Past:
84 Future/Past:
85 Future/Past:
86 Future/Past:
87 Sci-Fi Future: - $10 Billion
88 Future/Past:
89 Sci-Fi Future:
90 Future/Past:
91 Future/Past: - Crew Return Vehicle - X-38
92 Future/Past: X-38 Video
93 Future/Past:
94 Future/Past: - X-33 - VentureStar
95 Future/Past:
96 Future/Past:
97 Future/Past:
98 Future: - Delta IV Heavy
99 Future: - Delta IV Heavy
100 Future: - Shuttle Fly-back boosters
101 Future: - Hyper-X
102 Future: - X-37
103 Future: Ion Drive Video
104 Sci-Fi Future
105 Sci-Fi Future:
106 Sci-Fi Future:
107 Sci-Fi Future:
108 Sci-Fi Future: - Anti-matter
109 Sci-Fi Future: - Boussard Ramjet Fusion Propulsion
110 Sci-Fi Future: - Electrodynamic Tether
111 Sci-Fi Future: - Jovian Electrodynamic Tether
112 Sci-Fi Future: - Laser Propulsion
113 Sci-Fi Future: - Beamed Energy Propulsion
114 Sci-Fi Future: - Pulsed Detonation Rocket
115 Sci-Fi Future: - Space Based Laser Re-boost
116 Sci-Fi Future: - Plasma Rocket
117 Sci-Fi Future: - Plasma Rocket
118 Sci-Fi Future: - Space Elevator - Original concept as old as Mesopotamia: Biblical Tower of Babel and Jacob s Ladder - Five Critical Technologies (Source: MSFC Study) - High Strength Materials - Tension Structures - Compression Structures - EM Propulsion - Supporting Infrastructure - May Lower Launch Costs to <$10/kg!
119 Sci-Fi Future: - $10 Billion - To LEO or GEO? - LEO: Possible Today - Lower end just inside atmosphere - Space plane flies to lower end for cargo times the cargo lifted by SSTO - GEO: YR Time Frame: Years for enabling technologies - YR for actual construction
120 Sci-Fi Future:
121 Sci-Fi Future: - $10 Billion
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