2 A B C D E F G H J K L M N O P R S T Y

Apollo’s Goals

Apollo was the third United States human spaceflight program carried out by the National Aeronautics and Space Administration (NASA) done in the 1960s and 1970s.  Apollo was put into motion by president Kennedy. President Kennedy’s goal of demonstrating the superiority of the US political and economic systems over that of the Soviet Union in the Space Race was to be accomplished by this singular and significant achievement.

The Apollo program marked a series of firsts for the space industry and succeeded in landing the first humans on another celestial body, the Moon. Millions of people globally watched as Astronaut Neil Armstrong stepped off the ladder onto the surface of the moon and spoke the first words.  The program was active in the 1960s and early 1970s and was a national effort that consumed a large percentage of the national budget to accomplish.

Project Apollo’s goals went beyond landing Americans on the moon and returning them safely to Earth. They included:

  • Establishing the technology to meet other national interests in space.
  • Achieving preeminence in space for the United States.
  • Carrying out a program of scientific exploration of the Moon.
  • Developing human capability to work in the lunar environment.
Designation Date Return to Earth Success/Failure
AS-201 2/26/66 N/A Success
AS-203 7/5/66 N/A Success
AS-202 8/25/66 N/A Success
AS-204 (Apollo 1) 2/21/67 N/A Failure
Apollo 4 11/9/67 N/A Success
Apollo 5 1/22/68 1/23/68 Success
Apollo 6 4/4/68 N/A Partial Failure
Apollo 7 10/11/68 10/22/68 Success
Apollo 8 12/21/68 1/27/00 Success
Apollo 9 3/3/69 3/13/69 Success
Apollo 10 5/18/69 5/26/69 Success
Apollo 11 7/16/69 6/24/69 Success
Apollo 12 11/14/69 11/24/69 Success
Apollo 13 4/11/70 4/17/70 Failure
Apollo 14 1/31/71 2/9/71 Success
Apollo 15 7/26/71 8/7/71 Success
Apollo 16 4/16/72 4/27/72 Success
Apollo 17 12/7/72 12/19/72 Success

Rocket and Spacecraft

The concept for how to accomplish the Apollo mission was determined in 1962.  flight mode, lunar orbit rendezvous, was selected in 1962. New more powerful rockets were needed to accomplish the goals and NASA set upon the task to develop the Saturn IB for Earth orbit flights and the Saturn V for lunar flights.

The Apollo spacecraft was comprised of three-parts.  The first spacecraft: the command module (CM) served as the crew’s quarters and flight control section.  The service module (SM) provided propulsion and spacecraft support systems.  The CM and SM combined were referred to the CSM,  The final part of the spacecraft was the lunar module (LM) which itself was made of two parts: the separate descent and ascent stages, each with its own engine.  The LM would to take two of the three crew to the lunar surface, provide life support while on the Moon, and return them to the CSM in lunar orbit with the ascent stage.

Launch Vehicle Propellant Usage[1]
Apollo 11 Apollo 11 Apollo 11 Apollo 11 Apollo 12 Apollo 12 Apollo 12 Apollo 12 Apollo 13 Apollo 13 Apollo 13 Apollo 13 Apollo 14 Apollo 14 Apollo 14 Apollo 14
Burn Rate  Lb/Sec Burn Rate  Lb/Sec Burn Rate  Lb/Sec Burn Rate  Lb/Sec
Burn Burn Burn Burn Burn Burn Burn Burn Burn Burn Burn Burn
Start End Time Start End Time Start End Time Start End Time
S-IC Burn (sec) -6.4 161.63 168.03 -6.5 161.74 168.24 -6.7 163.6 170.3 -6.5 164.1 170.6
Oxidizer (LOX), lb 3,305,786 39,772 3,266,014 19,437.10 3,310,199 42,093 3,268,106 19,425.30 3,304,734 38,921 3,265,813 19,176.80 3,312,769 42,570 3,270,199 19,168.80
Fuel (RP-1), lb 1,424,889 30,763 1,394,126 8,296.90 1,424,287 36,309 1,387,978 8,250.00 1,431,384 27,573 1,403,811 8,243.20 1,428,561 32,312 1,396,249 8,184.30
Total, lb 4,730,675 70,535 4,660,140 27,734.00 4,734,486 78,402 4,656,084 27,675.20 4,736,118 66,494 4,669,624 27,420.00 4,741,330 74,882 4,666,448 27,353.20
S-II Burn (sec) 164 548.22 384.22 163.2 552.34 389.14 166 592.64 426.64 166.5 559.05 392.55
Oxidizer (LOX), lb 819,050 3,536 815,514 2,122.50 825,406 3,536 821,870 2,112.00 836,741 3,533 833,208 1,953.00 837,484 2,949 834,535 2,125.90
Fuel (LH2), lb 158,116 10,818 147,298 383.4 157,986 4,610 153,376 394.1 159,931 4,532 155,399 364.2 159,232 3,232 156,000 397.4
Total, lb 977,166 14,354 962,812 2,505.90 983,392 8,146 975,246 2,506.20 996,672 8,065 988,607 2,317.20 996,716 6,181 990,535 2,523.30
S-IVB 1st Burn (sec) 552.2 699.33 147.13 556.6 693.91 137.31 596.9 749.83 152.93 563.4 700.56 137.16
Oxidizer (LOX), lb 192,497 135,144 57,353 389.8 190,587 135,909 54,678 398.2 191,890 132,768 59,122 386.6 190,473 136,815 53,658 391.2
Fuel (LH2), lb 43,608 31,736 11,872 80.7 43,663 32,346 11,317 82.4 43,657 31,455 12,202 79.8 43,546 32,605 10,941 79.8
Total, lb 236,105 166,880 69,225 470.5 234,250 168,255 65,995 480.6 235,547 164,223 71,324 466.4 234,019 169,420 64,599 471
S-IVB 2nd Burn (sec) 9,856.20 10,203.03 346.83 10,042.80 10,383.94 341.14 9,346.30 9,697.15 350.85 8,912.40 9,263.24 350.84
Oxidizer (LOX), lb 134,817 5,350 129,467 373.3 135,617 4,659 130,958 383.9 132,525 3,832 128,693 366.8 136,551 5,812 130,739 372.6
Fuel (LH2), lb 29,324 2,112 27,212 78.5 29,804 2,109 27,695 81.2 29,367 1,963 27,404 78.1 30,428 2,672 27,756 79.1
Total, lb 164,141 7,462 156,679 451.7 165,421 6,768 158,653 465.1 161,892 5,795 156,097 444.9 166,979 8,484 158,495 451.8
Oxidizer-Fuel Ratio
S-IC Stage 2.32 2.343 2.324 2.355 2.309 2.326 2.319 2.342
S-II Stage 5.18 5.536 5.225 5.359 5.232 5.362 5.26 5.35
S-IVB Stage 1st burn 4.414 4.831 4.365 4.831 4.395 4.845 4.374 4.904
S-IVB Stage 2nd burn 4.597 4.758 4.55 4.729 4.513 4.696 4.488 4.71
[1]All times are referenced to Range Zero; all other values represent actual usage, in pounds mass. Sources are the Saturn V launch vehicle flight evaluation reports.

Chart from NASA. https://history.nasa.gov

 

Other interesting links to look over:

https://datastro.opendatasoft.com/explore/dataset/project-apollo-archive/table/?disjunctive.apollo_x&sort=apollo_x&refine.apollo_x=Apollo+9

https://history.nasa.gov/SP-4029/Apollo_18-11_Launch_Vehicle-Spacecraft_Key_Facts.htm