Current RLV Projects
Outside of USA
Past
RLV Projects...
Australia and New Zealand:
Chinese RLV(?):
Europe:
Articles and papers:
ACTS ((Advanced
Crew Transportation System) - joint ESA/Russia
program
Next
generation launchers - ESA
FAST20XX - Future High-Altitude High-Speed
Transport (FAST) 20XX -
Study of suborbital and hypersonic point-to-point
transport systems
Spaceliner:
LAPCAT (Long Term
Advanced Propulsion Concepts and Technologies)
FLACON:
Future High-Altitude Flight - an Attractive Commercial
Niche? - Europa. EU Projects
Survey
report on space tourism - Sam Adlen of the
Vega
Group .
ESA
-Next generation launchers
ARD - capsule launched to test thermal protection
systems.
Ares - Atmospheric Reentry Experimental
Spaceplane
Themis
Tarantis
ARIES - Thales Alenia concept
Spacelinq.nl
- A Dutch suborbital spaceplane project derived
from the US Rocketplane.
BOOSTER
Space Industries - European company planning
an air-launched suborbital rocketplane
Bristol
Spaceplanes
Dassault Aviation
VEHRA
EADS Astrium
Space Tourism Vehicle
DSL
EADS/DASA/Astrium - Alpha/Phoenix/Hopper
- ASTRA
Germany's reusable sub-orbital Hopper demonstrator.
CIRA Hopper
Orbspace
- Austrian based startup that plans to build a
VTOVL suborbital vehicle.
Infinity
would go to an altitude of 200 km and could
be configured for manned or unmanned operations.
The small prototype
JetFly
would provide a testbed for development of
technologies for the Infinity.
PRORA
- Italy - National Program for Aerospace Research
-RLV technology development program
Pollux
USV
(Unmanned Space Vehicle) - Castor
IXV - atmospheric reentry
demonstrator, which has a small lifting body
design, will fly to space on a Vega launcher
in 2012:
AREV
(select AREV under "text capability"
list): Atmospheric Re-entry Experimental Vehicle
Pre-X - France
Project
Enterprise - A privately funded project involving
an alliance of the TALIS-Institute ,
Swiss Propulsion
Laboratory (SPL), VEGA ,
and Xtreme
Air GmbH .
Talis
Enterprise AG
Project Enterprise new debut - Space Transport
News - Feb.14.08
This project began in 2006 and was redefined
in 2008. Involves a horizontal takeoff and
landing vehicle for space tourism.
Plan is to first build a prototype "Black
Sky“rocket powered version of an existing
Xtreme airframe. This will begin flying
in 2010
Maiden flight of the production model
"Enterprise" is planned for 2011
The goal is by 2013 to see wo flights
per week with 3 passengers each.
Articles:
Earlier design:
Rocket
Designers Look To The Next Generation
SKYLON
- Reaction Engines
SpaceFleet
StarChaser
SPL - Swiss Propulsion
Laboratory - non-profit group, university
based
XBow
II - 2 stage reusable suborbital with
lift-off-mass of ~1500kg, powered by LOX/kerosene
engines on both stages.
XBow
III - 3 stage reusable vehicle of placing
small payload in LEO
Vehra-SH - lifting body, airlaunched concept
developed at Dassault Aviation
Rocket
Camera Platforms - Aairborne Engineering
These rocket powered vehicles resemble those
in the Lunar Lander Challenge in that they
hover and are fully reusable.
ESA Crew Vehicle - conventional capsule designs
India
RLV-TD (Technology Demonstrator)
Avatar
Scramjet research
General
.VIDEO .
Japan's RVT
(Reusable Vehicle Test) rises vertically
a short distance and then returns for landing. From
June 25, 2001.
Press release info available at Spaceref.com .
Japan
Flying
Vehicle technologies - ISAS
LIFLEX - Lifting Body Flight Experiment
ISAS
- RVT
RVT Successor - Reusable Sounding Rocket
Development
Status of Reusable Rocket Engine - Yoshida
et al, 2008 (pdf)
Abstract:
Test Results of Critical Elements for Reusable
Rocket Engine, Yoshida et al, July.08 (pdf)
Look
out Jeff Bezos, here comes JAXA's reusable
rocket! - Hyperbola - Apr.30.08
Ddiscussed
by Hiroyuki Ogawa of JAXA during a session
of the International
Personal Spaceflight Symposium in Las
Cruces, NM in October 2007.
CNET
- Japan story - May.21.07 - translated
A
Concept & Readiness To The Reusable Sounding
Rocket - Yoshifumi Inatani - ISAS/JAXA - May.2007
Slides about the RVT and its successor -
JAXA - translated version [link broken]
New vehicle would be 10.5m tall, 3m
diameter, 8,857kg GTW, 2619kg dry mass.
4 31kN engines, 315sec specific impulse.
National Aerospace
Lab:
JAXA
Kankoh Maru
PD
Aerospace
Private company planning a sounding rocket
and then manned suborbital
Korea
C&Space
- suborbital Proteus vehicle.
Russian/Soviet Reusable
vehicles
RLV Supporting Technology
Pad Abort Demonstration
(PAD)
Rocket Engine Technology:
Barber-Nichols :
Composite Fuel
Tanks & Other Structures
Upper stages , i.e. for taking payloads
to GEO:
Upper stage planned for XCOR
Lynx
Upper stage planned for Scaled SpaceShipTwo
Thermal
Protection
Other Technology
Other RLV sections: