Some photos (from ebay) of a NASA PR glossy from December, 1961, showing the then-current Saturn C-5 configuration. Note the fairly obvious signs of some retouching of the engines on the first stage… either the engines were originally larger, or they were larger in number. Note the lack of the small but distinctive stabilizing fins on the first stage.
Somewhere north of 20 years ago I received a package in the mail from Martin-Marietta containing stuff on their then-current NIMF study. NIMF was a mangled acronym for Nuclear Rocket Using Indigenous Martian Fuel; basically a propellant tank, structure, landing gear and a nuclear rocket engine, to be used for landing a payload on Mars and for flying or hopping around. The propellant would be liquid carbon dioxide, easily compressed from the Martian atmosphere; the performance would be, by conventional liquid hydrogen nuclear rocket standards, reasonably awful, but it would be adequate to lurch back into Mars orbit or to do long range hops.
Two main designs seem to have been studied: a conical “ballistic” vehicle that would be a dedicated “hopper,” landing on its tail, and a winded vehicle that would land vertically in a horizontal attitude. This latter design was sent to me in the form of diagrams and five computer renders. The renders – early 1990’s vintage – came as viewgraph transparencies, clearly photographs of a computer monitor. The winged vehicle had simple shock absorbers for landing gear, terminating in dishes rather than wheels meaning that a rolling start or stop was impossible. The available information sadly doesn’t explain how the thing was supposed to land vertically.
The full-rez scans of the viewgraphs have been made available to APR Patrons in the 2016-01 APR Extras Dropbox folder. If you’d like to help out and gain access to this and many other pieces of aerospace history, please check out the APR Patreon.
A NASA illustration (probably from 1964-66) showing the Saturn launch vehicles planned for the Apollo program. Note that the Saturn Ib shows the Lunar Module ascent stage, sans descent stage. This could have led to some interesting mission possibilities.
The full-rez scan has been made available to APR Patrons in the 2015-12 APR Extras Dropbox folder. If you’d like to help out and gain access to this and many other pieces of aerospace history, please check out the APR Patreon.
USLP 03
Issue 03 of US Launch Vehicle Projects is now available (see HERE for the entire series). Issue #03 includes:
- Juno V/Titan/Nomad: A 1958 concept for a space launcher using an ICBM for upper stages
- Convair ATE Nova: A 1963 idea for winged airbreathing boosters
- B-70/Gemini: Using a bomber as a booster
- Phase II VTOHL Orbit-On-Demand: a 1985 concept for a relatively small two stage to orbit spaceplane
- NASA Lewis Saturn Ib/Centaur/Kick Stage: a high energy upper stage
- NASA MSC 042B/Titan IIIL6: a straight-winged orbiter atop a large Titan derivative
- Heavy Lift Titan: A large diameter Titan core with three Shuttle boosters
- Escher “Unshackled”: An unconventional idea for a lunar rocket
USLP #03 can be downloaded as a PDF file for only $4.25:
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Large format USBP drawings, Issues 10-12
The CAD drawings created for USBP reformatted and rescaled for 11X17 collected in a separate volume. Drawings have in some cases been corrected, improved and added to.
USBP 11X17 10-12 collects the diagrams created for issues 10, 11 and 12, including:
Boeing Model 464-34-3, Republic mach 7, Lockheed CL-1301-1, Convair WS-125A, Boeing 484-415, Martin Model 223-10, Boeing Model 814-1010 Dyna Soar, Martin Model 192-5, Boeing Model 464-40, Boeing Model 701-218, Northrop Nuclear flying wing, North American D118, Martin Model 223-11, North American Model 705-00-04, Bell/Martin 464L, Boeing B-1, Boeing Big Bird BB 6800, Boeing Model464-41, Douglas MX-2091-E, Boeing Model 701-238, Martin Model 223-12, Northrop Nuclear Flying Wing, Rockwell MRCC, Lockheed CL-820-8
USBP11x17-10-12 can be downloaded as a PDF file for only $11:
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Large format USBP drawings, Issues 13-15
The CAD drawings created for USBP reformatted and rescaled for 11X17 collected in a separate volume. Drawings have in some cases been corrected, improved and added to.
USBP 11X17 13-15 collects the diagrams created for issues 10, 11 and 12, including:
Ryan Model 162, Boeing Orbital bomb, Northrop Atomic Wing, Consolidated Vultee High Speed Flying Boat, Martin Model 189, Boeing Model 464-046, Curtis F-87C, Boeing Model 701-247, Lockheed WS 464L Dyna Soar, McDonnell WS 464L Dyna Soar, North American WS 464L Dyna Soar, Republic WS 464L Dyna Soar, Convair WS 464L Dyna Soar I, Convair WS 464L Dyna Soar II, Douglas WS 464L Dyna Soar, Northrop N206 WS 464L Dyna Soar, Boeing Model 814-1010 Dyna Soar II, Bell/Martin WS 464L Dyna Soar, Boeing Model 2050E Dyan Soar, Boeing Dyna Soar/ Titan IIIc, Bell D2001 TS-149, Lockheed Harvey; Convair Model 35, Rockwell D661-27, Boeing Model 464-49, Boeing Model 988-123, Boeing Manned Orbital Bomber, Boeing Model 701-251
USBP11x17-13-15 can be downloaded as a PDF file for only $11:
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DARPA Scraps Plan To Launch Small Sats from F-15 Fighter Jet
ALASA (Airborne Launch Assist Space Access) was a program to develop a launch vehicle that could be carried aloft by an F-15, with an orbital payload of around 45 kilograms. The design detail that was supposed to make ALASA work was what killed it: the propellant.
ALASA was to use liquid rocket engines. Nothing new there. The propellant combination was acetylene and nitrous oxide; that’s kinda new. But the Really New part of the design was that the two propellants were to be pre-mixed, meaning that the vehicle required only a single tank and simpler plumbing. Pre-mixing fuel and oxidizer is always a tricky proposition, but it has been successfully demonstrated from time to time. But here, in several tests the propellant simply exploded. This should not be overly surprising… acetylene is one of those unstable chemicals that will on occasion blow itself to bits just because it’s cranky. Mixing it with an oxidizer is just asking for trouble.
DARPA seems to have bailed on the launcher program, but is continuing to try to develop the propellant (called NA-7). Tricky though it may be, if it can be reliably stabilized there are undoubtedly vehicle designs that could effectively utilize it.
The ALASA vehicle made another unusual design choice: the rocket engines were near the front, not at the back. The reason for this: the trailing propellant tank could be dropped as a stage, but leave the engines in place. This would theoretically make the vehicle lighter, at the risk of having hot rocket exhaust scraping down the sides of the tank.
Now available… a new additions to the US Aerospace Projects series.
US Bomber Projects #17
USBP #17 includes:
M.C.D. 392: A wartime design for a global-range bomber
Martin Model 194: A strategic bomber somewhat larger than the B-29
Lockheed CL-285-815: A supersonic nuclear powered concept with five engines
Consolidated Model 36: An early design for the B-36 with twin tails
Boeing Model 701-290: A supersonic bomber on the road to the B-59
Thiokol 260-inch ICBM: An unreasonably large ICBM concept
ARFL ESAV: A recent concept for a stealthy supersonic bomber
Convair GEBO II: An ancestor of the B-58, carried aloft under a B-60
USBP#17 can be purchased for downloading for the low, low price of $4.25.
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Not exactly a “PDF” review, but this should be of interest to many here: “Missiles & Rockets” magazine, a weekly periodical published from 1958 into 1968, was much like Aviation Week except with a more specific focus. And it has been made available on archive.org. I’ve found the search function to be somewhat ineffective, but the system allows for fairly straightforward navigation along with easy downloading of individual pages as high-rez JPEGs. The collection is not complete, sadly; it doesn’t look like it’s being completed, but there are nevertheless a fair number of issues available.
https://archive.org/details/misslesandrockets&tab=collection
Much more aerospace stuff is available via the APR Patreon.
A three stage vehicle to transport 10 passengers to space stations and the like. I’ve recently come into possession of a whole bunch of reports on the Reusable Aerospace Passenger Transport and Reusable Orbital Transport programs; at some point these might make the makings of an APR article.
The third stage bears a vague similarity to the Boeing Dyna Soar in configuration, but is an entirely different vehicle. This concept helped set the course towards the Space Shuttle.