Episodes Tagged with "Jpl"
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
mySuperLamePic_c1194b7fa9498eb5af694d8530d3ebf8
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 February 26, 2015
John_Houbolt_and_LOR2
Earth Orbit Rendezvous
Apollo_Direct_Ascent
Posted on March 5, 2015
12-Second stage (S-IV)
11-Booster stage (S-I)
10-Proposed C-2
9-C-1 and earlier vehicles
8-Model of blockhouse at Launch Complex 34
7-Vehicles using Titan and Atlas stages
6-Saturn C
5-Saturn B
4-Preliminary concept of Launch Complex 34, Cape Canaveral
3-Early H-1 Engine
2-Thor-Jupiter engine
1-Proposed configuration of a clustered booster
Posted on March 26, 2015
two landing techniques proposed for the direct ascent mode
SA-1
RendezvousMethods
proposed lunar-surface-rendezvous procedure, a propellant-transfer vehicle takes fuel from the tanker to a manned space vehicle. After loading the fuel, the two astronauts would fire the engine of their spacecraft to return to the earth
Major configuration changes in the Apollo spacecraft from May 1960 to July 1962
Early design concepts of C-1 and C-5 versions of the Saturn launch vehicles
A ferry that would leave a command ship in orbit around the moon, visit the lunar surface, and then return to the command ship for the voyage back to the earth
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 May 23, 2013
ex1
ex
exlaunch
exlaunch1958
206601main_explorer-stand-516
206607main_launch-516
207199main_conference-516
206619main_pic-516
206623main_pickering-273
206689main_van-allen-516
206615main_medaris-516 (1)
Posted on May 30, 2013
Vanguard_1
Vanguard_rocket
Pioneer_I_on_the_Launch_Pad_-_GPN-2002-000204
Pioneer_1
Pioneer Satellite Replica
753px-Pioneer_3
Posted on January 21, 2016
6-Astronauts Pay a Visit to Surveyor 3
5-Photomosaic of a panorama taken by Surveyor 7 of its landing site
4-Surveyor 6 on the Plains of Sinus Medii
3-Wide-angle picture of the northwest wall of the Surveyor 5 crater
2-Surveyor_4_launch
1-Photograph of the Surveyor 3 spacecraft resting on the surface of the Moon, taken by Apollo 12 astronauts
Posted on October 31, 2013
space rocket history pic34
nasa_mariner2_float
Mariner_2_launch
Mariner_2_in_space
Diagram_of_Mariner_1_or_2_with_Atlas-Angena_launch_vehicle
413718main_g-64-1573
Posted on January 26, 2022
Posted on January 16, 2014
Cratered Hilands Mars
mariner04
Pickering-Johnson
Mariner_4_launch_2
Mariner Crater
20121209_Mars_Mariner_4_f840 Nasa
Posted on January 23, 2014
fig6 (1)McDonnell-proposed two-man Mercury spacecraft. Shown is the interior arrangement of spacecraft equipment
fig4
fig3
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 April 17, 2014
Sea of Tranquillity on the Moon from 11 km, 5 seconds before impact
Rilles on the Floor of Alphonus Crater
ranger8launch
ranger
Ranger 9
INTELSAT_I_(Early_Bird)
First picture of the Moon taken by Ranger 8
Delta_D_Intelsat1
Posted on January 29, 2015
c012a
GilruthThompsonGlennan
c010
c002c
c002b
c002a
Posted on February 5, 2015
glenn-kennedy_300_241_s_c1
ST-69-4-63
