space race

  1. Michel Van

    NAA Mars Exploration Module

    back in 1967 NAA made study NAS9-6464 for MEM for NASA They look into Lifting Body and Capsule shaped lander. last what was recommended Total mass of 64000 kg for 4 man 30 day stay on Mars The descent stage weight is 29207 kg with 13834 kg fuel The ascent stage weight is 16874 kg with...
  2. Triton

    Robert McCall space plane concept

    Artist's concept of United States Air Force space plane painted by Robert McCall found on eBay. Was this a real concept? Source: http://www.ebay.com/itm/Space-Shuttle-vintage-rare-US-Air-Force-Space-artists-concept-art-picture-/190614086223?pt=LH_DefaultDomain_0&hash=item2c617c224f
  3. Triton

    MSFC artist's concept for "Space Taxl" circa 1966

    Marshall Space Flight Center (MSFC) artist's concept for "Space Taxi" circa 1966. http://www.ebay.com/itm/1966-Vintage-NASA-8x10-Photo-Space-Taxi-Artists-concept-drawing-/110787704453?pt=LH_DefaultDomain_0&hash=item19cb763685
  4. Triton

    Artist's impression Space Station Mission Sequence circa 1963

    Artist's impression Space Station Mission Sequence circa 1963 found on eBay. Source: http://www.ebay.com/itm/1963-NASA-8x10-Photo-Artist-Concept-Space-Station-Mission-Sequence-/120821849104?pt=LH_DefaultDomain_0&hash=item1c218b1c10
  5. Triton

    Artist's impression Logistics Operations Mission Sequence circa 1963

    Artist's impression Logistics Operations Mission Sequence circa 1963 found on eBay. Source: http://www.ebay.com/itm/1963-NASA-8x10-Photo-Artist-Concept-Logistics-Operations-Mission-Sequence-/120821849910?pt=LH_DefaultDomain_0&hash=item1c218b1f36
  6. Michel Van

    NASA Space Station Concepts

    A BELLCOMM, INC. studie from July 23, 1968 by E. D. Marion J. A. Schelke they proposed an smaller Space Station concept against Skylab (and MOL)! Modules launch by Titan IIIM, with modified Gemini B capsule the module are 17 ft long and 15ft ø weight 21,200 to 12,100 lb Power system a 3 kw...
  7. Antonio

    Goodyear 3 stage rocket

    What is it? :o http://www.flickr.com/photos/sdasmarchives/6335602942/sizes/l/in/photostream/
  8. Graham1973

    Ranger 'X' - Lunar Flyby with film return capsule

    It seems that in 1962 the proposal was made to fit out what could have been 'Ranger 6' with a camera installation comprising the Ranger 3-4-5 vidicon unit paired with a high resolution (80ft at closest approach) film camera and a re-entry capsule that would drop the high resolution camera film...
  9. Grey Havoc

    Upper Atmosphere Research Satellite

    http://www.youtube.com/watch?v=5laK2JopaVE&feature=player_embedded NASA: Satellite won't fall on US (msnbc Cosmic Log) <a href="http://www.space.com/12899-nasa-falling-satellite-uars-space-junk-infographic.html"> <img...
  10. Graham1973

    Manned/Unmanned Lunar Explorer (MULE)

    Over the years NASA has run various systems engineering courses with universities around the United States. In the mid-1970 a group associated with Rice University was asked to design a Dual-Mode rover for use in the 1980's. The selected design was for a two man, tracked rover. Manned/Unmanned...
  11. J

    Space Stations launched by N1

    Th N1 rocketwas built back in the 60's by the USSR to put a man on the Moon, but I have read that it also had the goal of launching heavy military space hardware, including space stations, and putting it in Earth orbit. I konow the Almaz project and the Polyus satellite, but the former were...
  12. Graham1973

    Hughes/Sandia - Pioneer Mars Orbiter (1974)

    Concerned about the cost of Viking 1 & 2, NASA looked at lower cost alternatives for the 1977 & 1979 Mars launch opportunities . One of the proposed missions was to use a modified version of the Pioneer Venus Orbiter to carry six RTG powered penetrators to Mars. Once the spacecraft entered...
  13. Graham1973

    Bendix Dual Mode LRV

    During the 1960's one proposal for the Lunar Roving Vehicle (LRV) was make it so that after the manned mission was over it could be used as an unmanned rover for further exploration. Here is the final presentation report for the Bendix Version...
  14. Graham1973

    Rocketdyne (Rockwell) - 250-500k Aerospike Engine

    Just uploaded to the NTRS, a rather interesting study from the late 1960's The Aerospike Engine. Concept, Performance, Design & Operational Data. Liquid Hydrogen Propellants 250-500 KBLF Thrust Class http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900066185_1990066185.pdf
  15. Triton

    AAP Manned Single-Launch Venus Fly-by Mission (1967)

    Preliminary Mission Study of a Single-Launch Manned Venus Flyby with Extended Apollo Hardware, MSC Internal Note No. 67-FM-25, Jack Funk and James J. Taylor, Advanced Mission Design Branch, Mission Planning and Analysis Division, NASA Manned Spacecraft Center, Houston, Texas, February 13, 1967...
  16. Triton

    Lockheed Emergency Earth Orbital Escape Device (EEOED) 1969

    The Lockheed Emergency Earth Orbital Escape Device (EEOD) was a concept for a small capsule launched from a Titan/Agena booster or Saturn V that could be used to rescue the crew from an Apollo Applications Program (AAP)-based space station in Earth orbit, or permanently attached to such a...
  17. C

    Why not Apollo hardware for MOL?

    Why USAF not consider to use Apollo hardware for MOL? The military-spy station could be launched by Saturn IB ,or more large, by Saturn V. A MOL-Skylab type of station would be the advantage to be reusable for more that one mission. Instead of Gemini-B,the crew could be on Apollo capsule (with...
  18. Grey Havoc

    Martin Company 1959 Lunar Simulator

    From the June 1959 edition of Popular Science, an article on the Martin Company's USAF Lunar Simulator project, basically intended to simulate conditions inside a long-term manned installation on the Moon. Among it's interesting features was the plan to eventually have it house it's own...
  19. G

    Reusable One-stage Orbital Space Truck

    A Douglas Phil Bono concept circa December 1962. http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19770069308_1977069308.pdf
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