Human-rated re-usable spaceplane concept
VentureStar
Simulated view of VentureStar in
low Earth orbit
, having released its payload
|
Function
| Crewed Re-usable
Spaceplane
|
---|
Manufacturer
| Lockheed Martin
|
---|
Country of origin
| United States
|
---|
|
Height
| 38.7 m (127 ft)
[1]
|
---|
Diameter
| 39.0 m (128.0 ft)
[2]
|
---|
Mass
| 1,000,000 kg (2,200,000 lb)
[1]
|
---|
Stages
| 1
|
---|
|
|
Mass
| 20,000 kg (44,000 lb)
[1]
|
---|
|
---|
|
Status
| Cancelled
|
---|
Launch sites
| Kennedy
,
LC-39A
|
---|
Total launches
| 0
|
---|
|
|
Powered by
| 7
Rocketdyne RS-2200
Linear Aerospikes
[1]
|
---|
Maximum thrust
| 3,010,000 lbf (13.4 MN)
[1]
|
---|
Propellant
| LOX
/
LH2
[1]
|
---|
|
|
VentureStar
was a
single-stage-to-orbit
reusable launch system
proposed by
Lockheed Martin
and funded by the U.S. government. The goal was to replace the
Space Shuttle
by developing a re-usable
spaceplane
that could launch satellites into orbit at a fraction of the cost. While the requirement was for an uncrewed launcher, it was expected to carry passengers as cargo. The VentureStar would have had a wingspan of 68 feet (20.7 m), a length of 127 feet (38.7 m), and would have weighed roughly 1000
t
(2.2 million lb).
VentureStar was intended to be a commercial
single-stage-to-orbit
vehicle that would be launched vertically, but return to Earth as an airplane. Flights would have been leased to
NASA
as needed. After failures with the
X-33
subscale technology demonstrator test vehicle, funding was cancelled in 2001.
VentureStar was essentially a bigger version of the X-33 but was not produced.
[3]
The X-33 had ongoing problems meeting performance requirements for the carbonfibre hydrogen fuel tank.
[3]
There were a number of other technologies that were part of the program, including the linear
aerospike rocket engine
. One point of praise was the metallic thermal protection system developed by
BF Goodrich
.
[3]
Advantages
[
edit
]
VentureStar's engineering and design would have offered numerous advantages over the
Space Shuttle
, representing considerable savings in time and materials, as well as increased safety.
[4]
VentureStar was expected to launch satellites into orbit at about 1/10 the cost of the Shuttle.
Readying VentureStar for flight would have dramatically differed from that of the Space Shuttle. Unlike the
Space Shuttle orbiter
, which had to be lifted and assembled together with several other heavy components (a large
external tank
, plus two
solid rocket boosters
), VentureStar was to be simply inspected in a
hangar
like an airplane.
[4]
Also unlike the Space Shuttle, VentureStar would not have relied upon
solid rocket boosters
, which had to be hauled out of the ocean and then refurbished after each launch.
[4]
Furthermore, design specifications called for the use of linear
aerospike engines
that maintain thrust efficiency at all altitudes, whereas the Shuttle relied upon conventional nozzle engines which achieve maximum efficiency at only a certain altitude.
[4]
VentureStar would have used a new metallic thermal protection system, safer and cheaper to maintain than the ceramic protection system used on the Space Shuttle. VentureStar's metallic heat shield would have eliminated 17,000 between-flight maintenance hours typically required to satisfactorily check (and replace if needed) the thousands of heat-resistant
ceramic tiles
that compose the Shuttle exterior.
[4]
VentureStar was expected to be safer than most modern rockets.
[4]
Whereas most modern rockets fail catastrophically when an engine fails, VentureStar would have a thrust reserve in each engine in the event of an emergency.
[4]
For example, if an engine on VentureStar failed during ascent, another engine would shut off to counterbalance the failed thrust, and each of the remaining working engines could throttle up to safely continue the mission.
[4]
Unlike the Space Shuttle, whose solid rocket boosters produced chemical wastes, primarily
hydrogen chloride
, during launch, VentureStar's exhaust would have been composed of only water vapor, since VentureStar's main fuels would have been only
liquid hydrogen
and
liquid oxygen
.
[4]
This would have given VentureStar the benefit of being environmentally clean.
[4]
VentureStar's simpler design would have excluded
hypergolic propellants
and even
hydraulics
, relying instead upon electrical power for flight controls, doors and landing gear.
[4]
Because of its lighter design, VentureStar would have been able to land at almost any major airport in an emergency,
[4]
whereas the Space Shuttle required
much longer runways
than available at most public airports.
Cancellation
[
edit
]
The VentureStar program was cancelled due to development cost concerns accompanied by technical problems and failures in the
X-33
program, a program which was intended as proof-of-concept for some of the critical technologies needed by the VentureStar. The failure during a test of the X-33's complex, multi-lobe composite-structure cryogenic hydrogen tank was one of the main reasons for the cancellation of both the X-33 and the VentureStar. Ultimately, the VentureStar program required too many technical advances at too high a cost to be viable.
Program hardware
[
edit
]
Examples:
[3]
One of the technological barriers at the time was the hydrogen fuel tank.
[3]
One positive was that several years later the performance requirements for such a hydrogen tank were achieved, as NASA gained more experience with cryogenic carbon fiber fuel tanks.
[5]
September 7, 2004,
Northrop Grumman
and NASA engineers unveiled a liquid hydrogen tank made of carbon fiber composite material that had demonstrated the ability for repeated fuelings and simulated launch cycles.
[5]
The tank was a simple cylinder, not the complex shape used for the X-33. Northrop Grumman concluded that these successful tests have enabled the development and refinement of new manufacturing processes that will allow the company to build large composite tanks without an
autoclave
; and design and engineering development of conformal fuel tanks appropriate for use on a single-stage-to-orbit vehicle.
[6]
In fiction
[
edit
]
In the 2001 novella and 2015 novel
Lash-Up
by
Larry Bond
and Chris Carlson, the VentureStar prototype is converted into an armed spacecraft named
Defender
in order to protect US space assets from China, which is using a
space gun
to destroy
GPS satellites
.
[7]
[8]
In
John Varley
's novel
Red Thunder
and sequels, one of the major protagonists is a former VentureStar pilot.
In the television series
Star Trek: Enterprise
, an operational VentureStar spaceplane is included in the opening credits as part of the history of human spaceflight.
[9]
In the television series
Space Island One
, a fleet of VentureStars resupply the titular commercial space station.
Diagram
[
edit
]
See also
[
edit
]
References
[
edit
]
- ^
a
b
c
d
e
f
"AeroSpace Online:X-33 Advanced Technology Demonstrator"
. Retrieved
2007-04-23
.
- ^
"Venturestar"
. Archived from
the original
on December 28, 2016.
- ^
a
b
c
d
e
"X-33/VentureStar - What really happened"
. 4 January 2006.
- ^
a
b
c
d
e
f
g
h
i
j
k
l
"SP-4220 Wingless Flight: The Lifting Body Story (Chapter 9)"
.
R. Dale Reed (NASA Dryden Flight Research Center, Aerospace and Contract Engineer)
.
NASA
. August 1997
. Retrieved
January 21,
2010
.
- ^
a
b
Northrop Grumman.
"Northrop Grumman, NASA Complete Testing of Prototype Composite Cryogenic Fuel Tank"
,
News Releases
, September 7, 2004, accessed April 27, 2011.
- ^
Black, Sara (November 2005).
"An update on composite tanks for cryogens"
.
High-Performance Composites
.
- ^
Bond, Larry
(2001). "Lash-Up". In
Coonts, Stephen
(ed.).
Combat
.
New York
:
Forge
. pp. 149?265.
ISBN
0-312-87190-2
.
OCLC
45066376
.
- ^
Bond, Larry (2015).
Lash-Up
. With Chris Carlson. New York: Forge.
ISBN
978-0-7653-3491-6
.
OCLC
906798381
.
- ^
Archived at
Ghostarchive
and the
Wayback Machine
:
"Star Trek Enterprise Intro"
.
YouTube
.
External links
[
edit
]
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