We Land On The Moon

NASA artwork as it appeared in We Land On The Moon by John Raymond in 1963.

see also:

Beautiful scan of an original NASA issued lithograph.

and also:

Image credit: NASA
Image source: Mike Acs, Drew Granston, Numbers Station

Apollo 17 Experiments

Image credit: NASA
Image source: Numbers Station

Mercury Space Capsule

Image credit: ABMA
Image source: Numbers Station

Worden’s EVA

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It took me a few, but the lower version is either an earlier or later version of the same painting. The figure representing James B. Irwin is a repaint. My guess is the image on NASA’s site is later, reworked to give the figure a slightly more dramatic pose. The painting is by a North American Rockwell artist.

Image credit: NASA JSC
Images: NASA Images, Numbers Station

By Jove!

Jupiter Lunar Landing

From one of Jupiter’s 12 moons, earth astronauts gaze on this impressive, but bleak, view of the 86,900 mile-diameter planet. More than 316 times the mass of the Earth, Jupiter is seven times further from the sun than Earth; would require voyage of one to two months to reach at velocity of one million feet per second. Max Hunter, Douglas Aircraft Company engineer predicts economically feasible trips to Jupiter will be made through development of nuclear thrust spaceship engines. 

Douglas Aircraft Company, Inc. General Offices, Santa Monica, Calif.

Image credit: Douglas Aircraft Company
Image source: Numbers Station

Inside Deimos

ROMBUS

Configuration for a manned Mars mission (Project Deimos).

  1. Six man Mars landing capsule;
  2. Pressurized tunnel;
  3. Toroidal living compartment;
  4. Liquid hydrogen tanks (8);
  5. Spherical liquid oxygen tank
  6. Booster centerbody.

Project Deimos – Mars Landing Module

  1. Earth-return capsule;
  2. Command centre and pressurized tunnel;
  3. Separation joint, for return to Mars orbit;
  4. Mars landing propellant tanks(6);
  5. Ground access hatch;
  6. Mars-launch platform;
  7. Payload and power supply equipment compartment;
  8. Mars-launch propellant tank;
  9. Landing and take-off rocket motor;
  10. Jettisonable closure panel;
  11. Mars-entry heat shield;
  12. Extensible landing gear(4);
  13. Altitude-control system quads (4).

Frontiers of Space
Philip Bono & Kenneth Gatland
Macmillan, 1969

Image credit: Douglas
Image source: Numbers Station

Pegasus Cutaway & Plan

Pegasus Intercontinental Passenger Rocket

  1. Forward pressure dome;
  2. Two-man crew compartment;
  3. Re-entry stabilization fines (2);
  4. Cargo compartment;
  5. Aft pressure dome;
  6. Pressurized cabin for passengers (170);
  7. Deck structure (4) with passenger couches (43 each).

Pegasus during atmospheric re-entry uses the LH2-cooled plug nozzle as a heat shield. The ballistic transport would convey 172 passengers and freight 7,456 miles (12,000 km.) in 39 min. without exceeding an acceleration of 3g during ascent or re-entry. At the arrival spaceport it would hover on rocket thrust during a soft landing in the vertical attitude.

Pegasus Passenger Compartment

  1. Four-level passenger access doors (3);
  2. Stairways (2) connecting four passenger decks;
  3. Double-wall acoustic damping structure;
  4. Luggage racks (9);
  5. Re-entry stabilization fins (2).

Frontiers of Space
Philip Bono & Kenneth Gatland
Macmillan, 1969

Image credit: Douglas / Blandford Press
Images: Numbers Station, SDASM Archives

Concept by Henry Lozano Jr.

Image credit: North American Rockwell
Image source: Numbers Station

NAR Artist Concept

Image credit: North American Rockwell
Image source: Numbers Station