Barrington Bond said:In Wings And Space by John Chaplin SBN 7110 0150 2 Ian Allan Publishing is this picture...
circle-5 said:Wallpaper photo of Convair LACES Aerospaceplane model (ca. 1961).
archipeppe said:Many thanks Circle-5, and as follows my contribution about the matter as a part of Scott Lowther's APR old number (http://www.up-ship.com/eAPR/ev2n5.htm)circle-5 said:Wallpaper photo of Convair LACES Aerospaceplane model (ca. 1961).
Archibald said:In his seminal shuttle book Dennis Jenkins briefly mentions the HIRES scheme - Hypersonic Refueling ! does anybody knows a little bit more about that concept ?
circle-5 said:archipeppe said:Many thanks Circle-5, and as follows my contribution about the matter as a part of Scott Lowther's APR old number (http://www.up-ship.com/eAPR/ev2n5.htm)circle-5 said:Wallpaper photo of Convair LACES Aerospaceplane model (ca. 1961).
Thank you Archipeppe. I believe your drawing represents an earlier, development version of the Convair Aerospaceplane, with separate air intakes for the LACE oxygen separators (on three quadrants, behind the flight deck). It appears that Convair engineers were later satisfied with diverting enough air from the six hybrid engine intakes to perform that function. The fuselage intakes then became unnecessary. I've seen a model of your Aerospaceplane variant, but I do not have it, unfortunately.
No word on how the exposed ventral intakes would withstand atmospheric re-entry -- perhaps they were solid, unobtainium castings.
Barrington Bond said:I don't know any more than this...
shockonlip said:Archibald said:In his seminal shuttle book Dennis Jenkins briefly mentions the HIRES scheme - Hypersonic Refueling ! does anybody knows a little bit more about that concept ?
About HIRES specifically, no.
But, mid-air refuelling is just part of it.
LTV studied a more general capability they called Atmospheric Rendezvous in which mid-air refueling
was just one possibility. See AIAA paper 72-134 by Bird and Schaezler; "Aerospace Applications of
Atmospheric Rendezvous".
To give you an idea, of the application of these concepts, for example to a 2-stage orbital vehicle.
These concepts would permit the first stage or second stage to be designed and constructed without
certain low speed elements such as wings, landing gear, air breathing hypersonic, supersonic or
subsonic propulsion for cross range or ferry. Such vehicles would be received in atmospheric flight by
a carrier aircraft to perform those aspects of the mission. Significant reductions in gross lift off weight
are possible employing aircraft as a carrier or tow vehicle.
Interesting paper!
A Speculative Idea Beyond their baseline mode of operation, certain speculative operabonal modes exist that could signiticantly enhance the capability of APT vehicles in the future.
Consider the case where we have two Black Horse type vehicles, each using JP-5/H2O2 with an Isp of 335 s. The vehicles have a dry weight of 15,000 lb and a propellant load of 180,000 lb, which assuming a required Delta-v to orbit of 27 kft/s, allows them to deliver 1,000 lb to LEO.
Now, let's say that we fly the two of them off together, accelerating them jointly not to orbit, but rather to a suborbital trajectory with a velocity of 18.5 kft/ s. The two space planes are now outside the atmosphere, in free fall (i.e. zero gravity) in the immediate vicinity of each other. Let's say we now bring the two together and extend a refueling boom, allowing the 20,000 lb of residual propellant from one to be transferred to the other. The two then separate, the empty vehicle to return to Earth, the enriched vehicle to ascend to orbit with a payload of 12,000 lbs. Without any new hardware, the orbital delivery capability of the system can be increased by a factor of 12.
hesham said:The Republic Scramjet.
Michel Van said:Could be Lockheed System III from the Earth-to-space "shuttle" vehicles for NASA's Marshall Space Flight Center. around 1962-1964
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