Explore: Titan Launch Vehicles
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1RL10A-3-3A rocket engine modeling project
By Michael Binder
“RL10A-3-3A rocket engine modeling project” Metadata:
- Title: ➤ RL10A-3-3A rocket engine modeling project
- Author: Michael Binder
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“RL10A-3-3A rocket engine modeling project” Subjects and Themes:
- Subjects: ➤ Heat transfer - Computerized simulation - Launch vehicles - Propulsion - Heat of combustion - Turbomachinery - Rocket engines - Centaur launch vehicle - Atlas launch vehicles - Titan launch vehicles
Edition Identifiers:
- The Open Library ID: OL18118413M - OL17125078M - OL17565486M - OL15497475M
- Online Computer Library Center (OCLC) ID: 39715557
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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2Draft environmental impact statement for the Galielo Mission (Tier 2)
By United States. Office of Space Science and Applications. Solar System Exploration Division.
“Draft environmental impact statement for the Galielo Mission (Tier 2)” Metadata:
- Title: ➤ Draft environmental impact statement for the Galielo Mission (Tier 2)
- Author: ➤ United States. Office of Space Science and Applications. Solar System Exploration Division.
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Office of Space Science and Applications, Solar System Exploration Division
- Publish Date: 1988
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Draft environmental impact statement for the Galielo Mission (Tier 2)” Subjects and Themes:
- Subjects: ➤ Booster rocket engines - Environment effects - Environmental surveys - Galileo Project - Radiation hazards - Radioisotope batteries - Spacecraft launching - Spacecraft power supplies - Thermoelectric generators - Titan launch vehicles - Ulysses mission
Edition Identifiers:
- The Open Library ID: OL18239054M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Draft environmental impact statement for the Galielo Mission (Tier 2) at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Titan IV
Titan IV was a family of heavy-lift space launch vehicles developed by Martin Marietta and operated by the United States Air Force from 1989 to 2005.
Titan (rocket family)
launch vehicle versions contributed the majority of the 368 Titan launches, including all the Project Gemini crewed flights of the mid-1960s. Titan vehicles
Vandenberg Space Launch Complex 4
handle Titan rockets. The designation SLC-4 was applied at the time of the conversion to launch Titan launch vehicles. Both pads at Space Launch Complex
LGM-25C Titan II
The modified Titan II SLVs (Space Launch Vehicles) were launched from Vandenberg Air Force Base, California, up until 2003. Part of the Titan rocket family
HGM-25A Titan I
that were a part of the U.S. arsenal and space launch capability. The Titan I was unique among the Titan models in that it used liquid oxygen and RP-1
Titan IIIC
The Titan IIIC was an expendable launch system used by the United States Air Force from 1965 until 1982. It was the first Titan booster to feature large
Titan II GLV
The Titan II GLV (Titan II Gemini Launch Vehicle) or Gemini-Titan II was an American expendable launch system derived from the Titan II missile, which
Titan IIIB
Titan IIIB was the collective name for a number of derivatives of the Titan II ICBM and Titan III launch vehicle, modified by the addition of an Agena
Titan IIIE
The Titan IIIE or Titan 3E, also known as the Titan III-Centaur, was an American expendable launch system. Launched seven times between 1974 and 1977
Cape Canaveral Space Force Station
converted to service Delta IV launch vehicles. The Air Force chose to expand the capabilities of the Titan launch vehicles for its heavy lift capabilities