Tag: VTOVL

Pegasus Cutaway & Plan

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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).
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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.

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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

Selena Storyboard

How re-usable ROMBUS-type launch vehicles can be applied to construction of a temporary lunar base (Project Selena).

  1. Vehicle en route for the Moon is refuelled in Earth Orbit;
  2. Soft-lands on the Moon with lunar base components;
  3. Pressurized moon-tractor hauls hydrogen tanks adapted for human habitation to assembly site;
  4. The lunar base is ready for occupation.

Frontiers of Space is peppered with artwork from Douglas, including paintings by Don Charles and James Finnell. In the book, this section was illustrated with (pretty poor) knock-offs. Why? Who knows? These were the masters.

Image credit: Douglas
Image source: SDASM Archives

Deimos Storyboard

Mission to Mars (Project Deimos)

  1. Hydrogen tanks jettison as ROMBUS spaceship accelerates from Earth-orbit;
  2. Two hydrogen tanks jettison after retro-thrust into Mars orbit. Mars Landing Module separates from ROMBUS parent above the cratered deserts;
  3. After soft-landing, astronauts begin exploration setting out research equipment and taking meteorological soundings;
  4. Ascent stage of Mars Landing Module returns astronauts to ROMBUS parent in Martian orbit for return to Earth.

Frontiers of Space
Philip Bono & Kenneth Gatland
Macmillan, 1969

Image credit: Douglas
Image source: SDASM Archives

Don Charles

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Image credit: Douglas
Image source: SDASM Archives

Rocket of The Future (1963)

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(DN4) DALLAS, TEX. APR. 23 — ROCKET OF THE FUTURE — The Rombus rocket, capable of orbiting 500-ton payloads is shown in this artist’s drawing. Rombus and several other proposed future rocket concepts were described by John W. Stone, launch vehicles advanced studies manager for the National Aeronautics and Space Administration, at the Manned Space Flight Conference in Dallas today. Rombus would be more than 400 feet tall and 120 feet in diameter. The launch pad would be a water-filled basin. (AP Wirephoto) (ft31430ho) (For use with Howard Benedict story) 1963

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Image credit: Douglas
Images: Numbers Station, SDASM Archives