PROGRAMMABLE TECHNOLOGIES WEB SITE

A scientific study of the problems of digital engineering for space flight systems,
with a view to their practical solution.


Mirror of JSC History Site

as-506_tech_info_summary.pdf


Technical Information Summary
Apollo-11 (AS-506)
Apollo Saturn V Space Vehicle

S&E-ASTR-S-101-69
June 25, 1969
Marshall Space Flight Center

as202_saturn_Ib_results_vol_202.pdf


Results of the Third Saturn IB Launch Vehicle Test Flight
AS-202
Volume II

MPR-SAT-FE-66-13
October 25, 1966
Marshall Space Flight Center

saturn_v_payload_capability_082967.pdf


Saturn V LOR Payload Capability Commitment

Memorandum, August 29, 1967

apollo_04_technicalOinformation_summary.pdf  
apollo_05_saturn_v.pdf  
apollo_06_saturn_v.pdf  
apollo_07_saturn_v.pdf  
apollo_08_saturn_v.pdf  
apollo_09_saturn_v.pdf  
apollo_10_saturn_v.pdf  
apollo_11_flight_plan_july_1_1969.pdf  
apollo_11_saturn_v.pdf  
apollo_12_saturn_v.pdf  
apollo_13_saturn_v.pdf  
apollo_14_saturn_v.pdf  
apollo_15_saturn_v.pdf  
apollo_16_saturn_v.pdf  
apollo_17_saturn_v.pdf  
apollo_2004_Saturn_v.pdf  
apollo_acronym_guide.pdf  
apollo_program_summary.pdf  
as11pao.pdf  
as201_launch_results.pdf  
as202_saturn_Ib_results_vol_2.pdf  
as203_launch_results.pdf  
as-506_tech_info_summary.pdf  
flight_controllers.pdf APOLLO 201 NEWS CENTER

NASA Manned Spacecraft Center, Houston, Texas

NEWS RELEASE NO. 1 February 23, 1966

SUBJECT: Apollo/Saturn 201 Flight Controller and Recovery Assignments

200 pages

lm5_structures_handout.pdf  
mcc_operational_configuration_as15.pdf  
results_of_saturn_I_sa3_launch.pdf  
results_of_saturn_I_sa7_launch.pdf  
results_of_the_third_saturn_Ib_launch_vehicle
_test_flight_as_203.pdf
 
sa03_flight_evaluation_vol_1.pdf
(174 pages)

sa03_flight_evaluation_vol_2.pdf
(201 pages)

GEORGE C. MARSHALL SPACE FLIGHT CENTER

MPR-SAT-63-1

SATURN SA-3 FLIGHT EVALUATION

By Saturn Flight Evaluation Working Group

(U) ABSTRACT

The evaluation of the Saturn SA-3 test flight is presented in two volumes. The first volmne contains the results of the early engineering evaluation and the second volume contains supporting information and information related to the evaluation of the flight. In these volumes the performance of each major vehicle system is discussed with special emphasis on malfunctions and deviations. The SA-3 flight test was a complete success with all missions of the test being accomplished. No major malfunctions or deviations which would be considered a serious system failure or design deficiency occurred.

sa06_launch_results.pdf  
sa08_launch_results.pdf  
sa09_launch_results.pdf  
sa10_launch_results.pdf  
saturn_sa1_flight_evaluation_121461.pdf  
saturn_v_payload_capability_082967.pdf  
skylab_I_saturn_v.pdf

Saturn V Launch Vehicle Flight Evaluation
Report-SA-513
Skylab-1

MPR-SAT-FE-73-4
August 1, 1973
254 pages

skylab_II_saturn_Ib.pdf

Saturn IB Launch Vehicle Flight Evaluation
Report-SA-206
Skylab-2

MPR-SAT-FE-73-3
July 23, 1973
230 pages

skylab_III_saturn_Ib.pdf

Saturn IB Launch Vehicle Flight Evaluation
Report-SA-207
Skylab-3

MPR-SAT-FE-73-5
October 8, 1973
246 pages

skylab_IV_saturn_v.pdf

Saturn IB Launch Vehicle Flight Evaluation
Report-SA-208
Skylab-4

MPR-SAT-FE-74-1
January 31, 1974
251 pages

tape079.mp3  

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Last Revised: February 03, 2010
Digital Engineering Institute
Web Grunt: Richard Katz