ISAS Reusable Rocket Completes 2nd Flight Test Series
Aiming towards in-flight engine restart
by Patrick Collins
The reusable
VTOL
rocket developed and first flown in 1999 at the Institute for Space and Astronautical Science
(ISAS
) in Japan has been upgraded and reflown successfully.
Photographs of the vehicle under preparation in-flight are available at www.isas.ac.jp/dtc/saisiyo/saisiyo.html#return1. Quicktime videos of two of its three flights are available at www.isas.ac.jp/dtc/saisiyo/rvt6.mov and www.isas.ac.jp/dtc/saisiyo/0625rvt6-42.mov.
Only 3 metres tall, the vehicle nevertheless uses a liquid hydrogen fuelled engine, and was designed for operability - quick turnround, easy maintenance and check-out. Its current configuration is intended to fly eventually to 100 metres altitude from where it will perform an inflight engine shut-down and restart. It is a key requirement for VTOL
rockets that they be able to restart their engines for landing while falling through the atmosphere after re-entry.
In a recent interview in Space News
(July 9), Dr Inatani described the project as being a step towards the
Kankoh-maru
vehicle designed for space tourism by a team in the
Japanese Rocket Society
.
The ISAS
' vehicle is currently the only reusable
VTOL
rocket vehicle in the world - since NASA cancelled the DC-XA
project in 1995 after it had flown successfully a dozen times, having spent some $40 million on the project which it inherited from the US Department of Defence. Instead, Nasa has spent $1.3 billion on the X33
and X34
projects, neither of which ever even flew before being scrapped. The US government has rewarded this delinquent behaviour by giving NASA an additional $5 billion to spend on its "Space Launch Initiative" which will be as ineffective as the X33
and X34
in reducing launch costs.
Photographs of the vehicle under preparation in-flight are available at www.isas.ac.jp/dtc/saisiyo/saisiyo.html#return1. Quicktime videos of two of its three flights are available at www.isas.ac.jp/dtc/saisiyo/rvt6.mov and www.isas.ac.jp/dtc/saisiyo/0625rvt6-42.mov.
Only 3 metres tall, the vehicle nevertheless uses a liquid hydrogen fuelled engine, and was designed for operability - quick turnround, easy maintenance and check-out. Its current configuration is intended to fly eventually to 100 metres altitude from where it will perform an inflight engine shut-down and restart. It is a key requirement for VTOL
In a recent interview in Space News
The ISAS