Episodes Tagged with "Manned Spacecraft Center"
Posted on February 12, 2015
Using a model at upper left, William Rector of General Dynamics Corp. describes the design his company proposed for the Apollo lunar mission
Spacecraft modules in this drawing were identified in the Space Task Group’s request for proposals from contractors for developing and producing the command module
Saturn 1 test
Saturn 1 test 2
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At lower left, E. E. Clark and Carlos de Moraes of the Martin Company display three of a dozen command module configurations considered before the choice of the one to the right
ASA’s second Administrator, James E. Webb (at center above), and George M. Low (right above) of NASA Headquarters receive a model of General Electric’s proposed vehicle
Posted on February 19, 2015
David G. Hoag, technical design director at the laboratory, examines the inertial measuring unit that would measure changes in Apollo spacecraft velocity when propulsion systems were fired
MIT Instrumentation Laboratory Director C. Stark Draper inspects a mockup of the Apollo guidance and control system in the September 1963
astronaut positions
Posted on April 2, 2015
Early design concepts of C-1 and C-5 versions of the Saturn launch vehicles
NASA announced selection of the lunar-orbit-rendezvous landing technique at an 11 July 1962 press conference. left to right James E. Webb, Robert C. Seamans, Jr., D. Brainerd Holmes, and Joseph F. Shea
Harry C. Shoaf (Space Task Group Engineering Division 15 November 1961 of a proposed lunar lander to be used with an advanced version of the Mercury spacecraft
concept of a small lunar lander during descent to the surface of the moon, as proposed by Langley Research Center employees in October 1961
Posted on April 9, 2015
Shea uses models to demonstrate how the lunar module would dock with the command module
Rocket Comparison
Lunar orbit insertion
Posted on April 16, 2015
REF: 2-903-6 SA-2 LAUNCH AT CAPE. IGNITION OF ROCKET (SATURN 1 VEHICLE)
SA-2 erected on launch pedestal
Wernher_von_Braun_confers_with_Brainerd_Holmes_and_Nicholas_Golovin
Posted on April 23, 2015
The impact facility at North American was used to drop-test the CM
Selection of Little Joe II completed the Apollo family of launch vehicles.
Scott Carpenter, John Glenn, and Walter Schirra in 1963 inspect a full-scale mock up of the Apollo CM
North American Aviation Stormy,
Interior of a partial full-scale mockup of the Apollo command module
major parts of the command module structure
Posted on April 30, 2015
Posted on May 7, 2015
General Electric employees monitor activities of a spacecraft test in the automatic-checkout-equipment spacecraft control room in 1965
comparison of spacecraft and launch vehicle configuration
Apollo tracking network in 1966. Radar stations with large antennas for continuous tracking and communications were at Goldstone, California; Madrid, Spain; and Canberra, Australia
Posted on May 14, 2015
Full-scale model of the command module, above- the strake aerodynamic devices may be seen at either side of the spacecraft just above the aft heatshield
Removing LM from S=IVB stage
On 16 November 1963 in Cape Canaveral’s Blockhouse 37, NASA’s new manned space flight chief George Mueller
Communications with the moon as the earth turned. Astronauts on the moon’s surface also could talk to one another
Posted on May 21, 2015
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The cabin section (or primary structure) of the CM is assembled at North American in 1965
The CM probe would slip into the LM’s dish-shaped drogue, and 12 latches on the docking ring would engage, to lock the spacecraft together, airtight
Full-scale model of the service module, resting on a mockup of a spacecraft-lunar module adapter, with panels off to reveal part of the internal arrangement
Jettison of the launch escape system (right) after successful launch, also pulls away the boost protective cover that protects the windows from flame and soot
On the drawing of the launch escape system at upper right, the canard aerodynamic devices are near the top of the escape tower
Posted on May 28, 2015
VonBraunMuellerReesSA6
SA5_launch
sa-6-spacecraft
sa-6-dem
SA-6 spacecraft and launch vehicle ready to go
SA-6 on pad
SA-5Section cuts
SA-5
SA-5 S-IV stage
SA-5 on pad
SA-5 Demensions
apollo_sa7_launch
apollo_sa4
Posted on June 11, 2015
6-NASA engineers in 1964 decided that astronauts could stand in the lunar module cabin during the trip to the lunar surface. Note triangular windows
7-Proposed sleeping positions for astronauts on the moon
5-Mockup of lunar module cabin with seats
4-The drawing of the stage indicates positions of components
3-underside of the lunar module descent stage shows fuel tank installation
2-Administrator James Webb examines models of the lunar and command modules in docked position
1-Lunar module generations from 1962 (above left; the vehicle originally proposed by Grumman) to 1969
Posted on June 17, 2015
3-improved lunar module features – ladder, porch, hatch, and rendezvous window
2-he addition of a ladder on a landing gear leg made the task much easier
1- Astronauts found a knotted rope from the lunar module difficult to climb down (or up)
Posted on July 2, 2015
5-Removing the LEM
4-ApolloSpacecraftLMAdapterDiagram
3-Apollo_Spacecraft_diagram
2-Tm-1 mockup of the Lunar Module
1-lm-6-rendezvous-radar-antenna-assy-sm
Posted on July 9, 2015
4-SIV-SIVB
3-Saturn 1b-V
2-Cutaways
1- SIV_rocket_stage
Posted on July 16, 2015
4- Saturn_SA10_launch
Saturn_SA8_launch
2- The SA-9
8- Pegasus_Deployment_sequence
7- Cutaway views show the interior of the command module (for clarity, the center couch is not shown)
6- Pegasus Deployed
5- Pegasus Stowed
4- Saturn_SA10_launch
Posted on July 23, 2015
3- 1230_Lunar_module_LTA-2_R
2-Disher_John_
1-Lunar_Module_diagram
Posted on July 30, 2015
2-NASA_Group_1_and_2_Astronauts_Photo_With_Autopens
2-Back row- See, McDivitt, Lovell, White, & Stafford. Front row- Conrad, Borman, Armstrong, & Young
1- Project_Mercury_AstronautsBack row- Shepard, Grissom, Cooper; front row- Schirra, Slayton, Glenn, Carpenter.
Posted on August 5, 2015
Group4Astronaut
4-Group 4 L-R- Garriott, Gibson. Front row, L-R- Michel, Schmitt, Kerwin.
3-Astronaut_Group_Three_-_GPN-2000-001476
Posted on August 13, 2015
5-Back row, from L-R- Swigert, Pogue, Evans, Weitz, Irwin, Carr, Roosa, Worden, Mattingly, Lousma. Front row, from L-R- Givens, Mitchell, Duke, Lind, Haise, Engle, Brand, Bull, McCandless
Posted on August 20, 2015
AS-203_launch
AS-202_launch
AS-201_launch
Apollo-Saturn 201 mission – launch, recovery
Posted on August 27, 2015
3-Christopher_Kraft,_flight_director_during_Project_Mercury,_works_at_his_console_inside_the_Flight_Control_area_at_Mercury_Mission_Control
2-Wally Schirra (right) consults the flight plan for his Mercury-Atlas-8 (MA-8) mission with Flight Director Chris Kraft
1-Chris Kraft and Rober Gilruth
Posted on September 3, 2015
3-Robert F. Thompson (center) and Christopher C. Kraft Jr. (right) brief Rear Admiral W.C. Abhau
2-Kraft with his new flight directors before the Gemini 4 mission Clockwise from lower right Kraft, Gene Kranz, Glynn Lunney and John Hodge
1-Kraft Kranz Gemini Fuel Cell problem
Posted on September 10, 2015
3-Kranz and his teacher Kraft
2-Kranz at his console on May 30, 1965, in the Mission Operations Control Room, Mission Control Center, Houston
1-Kranz-F86 Sabre Cat
Posted on September 17, 2015
3-Astronauts Grissom, Chaffee, and White check the communications headgear in preparation for what was to have been the first manned Apollo flight – Apollo-Saturn 204, scheduled for 21 February 1967
2-CM-012 – Apollo One- arrives at Kennedy Space Center, 26 August 1966
1-Command module 012 and service module 012 in workstands at the North American Aviation plant, Downey, in 1965
Posted on October 1, 2015
Chaffee, White, and Grissom
apollo1-sketch-jg
the-Apollo-1-launch-pad-fire-that-killed-astronauts-Gus-Grissom-Roger-Chaffee-and-Ed-White-celebrities-who-died-young-31704639-1372-740
Posted on October 8, 2015
3-Apollo_1_patch
2-apollo1chaffee
1-Chaffee at the consoles in Mission Control during the Gemini 3 mission
Posted on October 15, 2015
1-1024px-AS-204_-_hatch
3-PrimeandBackupCrews
2-PrimeCrewAltitudeChamberTest
Posted on October 22, 2015
3-apollo
2-c216a
1-Apollo_1’s_Command_Module_-_GPN-2003-00057
Posted on October 29, 2015
CM parts were studied and catalogued in the Pyrotechnics Installation Building at Kennedy Space Center.
The CM wiring harness goes through x-ray inspection.
apollo-1-disassembly
Posted on November 5, 2015
Deputy Administrator Seamans, Administrator Webb, Manned Space Flight Administrator George E. Mueller, and Apollo Program Director Phillips testify before a Senate hearing on the Apollo accident
2-Apollo1Langley
1-Apollo1 Inve
Posted on November 12, 2015
LC34_memorial_benches
LC34plaque2 (1)
KSC_Launch_Complex_34
Apollo1plaque
Apollo_1_Silver-Colored_Fliteline_Medallion_(Flown_on_Apollo_9)
Posted on January 30, 2014
The operating principle of the fuel cell designed by General Electric, adopted for use in the Gemini spacecraft
modified Titan II booster
Gemini spacecraft to be released publicly
Adapter Section of Mark II
Four stages in a rendezvous mission as conceived early in 1962
An artist’s version of the use of ejection seats to escape from the Gemini spacecraft
fig8 proposed lunar lander to be used with an advanced version of the Mercury spacecraft
Posted on February 6, 2014
The general arrangement of liquid rocket systems (OAMS and RCS) in the Gemini spacecraft
Gemini landing gear part of the land landing system along with the paraglider
fig41The B. F. Goodrich partial-wear full-pressure suit being developed for the Gemini program
fig33Figure 33. The emergency parachute recovery system for the half-scale paraglider flight test vehicle for Phase II-A of the development program – Copy
fig27Gemini spacecraft nomenclature – Copy
Agena B
Posted on February 12, 2014
fig58 Astronauts after a training session in desert near Stead Air Force Base, Nevada
Goal
fig54 Instrumented mannequin being lowered into a boilerplate Gemini spacecraft in preparation for a dynamic sled test of the Gemini ejection system
fig52 Gemini launch vehicle 1 undergoing tests in the vertical test facility at Martin’s Baltimore plant
fig51 POGO suppression equipment proved out in the Titan II development program
fig48 Proposed deployment sequence for the ballute stabilization device
fig47 Titan II flight N-15 was launched from Cape Canaveral on January 10, 1963
Posted on February 27, 2014
Tang
space rocket history pic69
Gemini1-1
Gemini Launch
Gemini 1 Left Instrument Pallet
Gemini 1 Experiment Pallets
Posted on November 13, 2014
p-1G12Patch
LovelAldrinRecovery
Gemini12Into Sun
gemini_xii_mission
Posted on January 29, 2015
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GilruthThompsonGlennan
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c002a
Posted on February 5, 2015
glenn-kennedy_300_241_s_c1
ST-69-4-63
