My dear Hesham this stuff seems to be more AFRL rather than Dynasoar related....From Air Force 1964.
Hi Greenmartian,Hesham, could we obtain a higher-rez version of this Air Froce 1962 image you posted? Let me know. Thanks.
You can ask my dear Orionblamblam (Scott),maybe he has it ?.Hi can anyone help me with finding information on the 814-2014 dyna-soar I think it was a smaller version I am looking for a 3 view Thanks
The Dyna-Soar that had unaerodynamic ribbing puzzles me.
SR-71 had it tooThe Dyna-Soar that had unaerodynamic ribbing puzzles me.
Are these from a video ?X-20 flight.
Nugo, I've noticed that in your various posts, you use the "?" to indicate a missing figure in your designations. However, this is misleading because it could indicate a designation you're not sure about.
For example, when you write "Lockheed Model CL-4??" my first impression is that you are questioning the fact that it was called Model CL-4... when in fact you simply want to indicate the fact that the missing designation was in the 400 to 499 range...
May I suggest you replace the question marks by asterisks as follows:
Boeing/Vought Model 844/Vought Model 4**
Convair Model **
Douglas Model 1***
Lockheed Model CL-4**
Martin/Bell Model 3**/Bell Model D-1** or D-2**
McDonnell Model 1**
North American X-15B (Model ***)
Northrop Model 1** or Model 2**
Republic Model AP-**
Model No. | Series Letter | Customer | Type Designation | Description | Date No. Assigned | Job Order |
---|---|---|---|---|---|---|
132 | A | USAF (IFGMP 1-3-58) | Aerial Test Vehicle | Conceptual Test Vehicle for DYNA SOAR I Program, Boost-Glide type Single-place, Low Wing, Span: (S), Length: (S), Inertial Navigation System, Automatic & Manual Flight Control System, Landing Skids & Parachute System, Provisions for different equipment configuations. Mod. Atlas Booster Solid-Prop. Rockets Bristol-Orpheus, Turbo-Jet (McDonnell Report 6006) | 2-18-58 | 6010-002 |
B | " | Aerial Manned Vehicle | Aerial Manned Vehicle for DYNA SOAR II Program, Boost-Glide type, Single Place (Two-Place Alternate Arrangement), Low Wing, Span: (S), Length: (S), Inertial Navigation System, Automatic & Manual Flight Control System, Landing Skids. Provision for Reconnaissance, Bomber, or Reconnaissance-Bomber Mission Equipment. Mod. Atlas Booster, Altered Navaho Boosters, Solid-Prop. Low Wing Rockets (McDonnell Report 6006) | " | " | |
C | " | Aerial Manned Vehicle | Aerial Manned Vehicle for DYNA SOAR III Program, Boost-Glide type, Single Place (Two-Place Alternate Arrangement), Low Wing Span: (S), Length: (S), Inertial Navigation System, Automatic & Manual Flight Control System, Landing Skids. Provision for Improved Reconnaissance, Bomber, or Reconnaissance-Bomber Mission Equipment. Mod. Atlas Booster "C" Boosters Solid-Prop. Rockets (McDonnell Report 6006) | " | " |
Not a Dyna Soar; entirely too large. A contemporary space logistics vehicle.I found this on the Facebook page "Vault of The Atomic Space Age". Does anyone know if this was an actual Dyna-Soar proposal.
i think it may be SLOMARI found this on the Facebook page "Vault of The Atomic Space Age". Does anyone know if this was an actual Dyna-Soar proposal. And if so, from which company? The comments didn't yield any clues and Google image search wasn't of much help.
Probably related:...interesting item in a case at the Vought Retired Employees archives.
This was not a high-speed model as it appeared to have been made with blown plastic. This is only the nose section of a larger model. (No. I did not see the rest of the model.) I have no information of the model number. Additional pictures may follow later.
LTV personnel have been actively associated with the development and application of air and space crew safety escape and rescue equipment for more than 20 years. This background of experience covers the early application of ejection seats to naval aircraft. It includes the pioneering development of a pilot escape capsule for the Navy, figure 1, and orientation of the initial escape capsule for the Boeing Dyna-Soar team, figure 2. This latter effort included complete responsibility for the first 200" of the Dyna-Soar glider including the integrated pilot control compartment and crew escape module. This program provided early experience in integrating normal and emergency life support and spacecraft control and display equipment to insure redundant capability by multiple functional use of system elements.
It wasn't the same engine. They were "based" on the AJ-10. Like S-IVB was based on the S-IV stage or 737 family
Dyna Soar was going to use an SRM for airlaunch.
...Check pdf 10301865, page 13.
Restored linkThank you Dynoman.
LC-33Before 1961 and the switch to orbital and Titan III, DynaSoar was to ride a Titan II from the Atlantic Missile Range.
I presume it would have launched from one of the three Titan II pads there : LC-15, LC-16 or LC-19 ? Any clue ?
Martin study for USAF on Titan II booster for Dyna-Soar Step I (DS-I).
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19740077029_1974077029.pdf