50mm cavity diameter solar thermal thruster made of single crystal molybdenum

Morio Shimizu; Hitoshi Naito; Hironori Sahara; Tadayuki Fujii; Hiroo Yugami; Ken Ichi Okamoto; Shigehiko Takaoka

doi:10.2514/6.2001-3733

50mm cavity diameter solar thermal thruster made of single crystal molybdenum

Morio Shimizu, Hitoshi Naito, Hironori Sahara, Tadayuki Fujii, Hiroo Yugami, Ken Ichi Okamoto, Shigehiko Takaoka

ENG - Mechanical Systems Engineering

Research output: Contribution to conference › Paper › peer-review

3 Citations (Scopus)

Abstract

This paper shows design, fabrication and experimental results of a large (50mm) cavity diameter windowless type of solar thermal propulsion (STP) thruster made of single crystal molybdenum (SCM) with tungsten chemical vapor deposition (W-CVD) coating. The nitrogen or helium propellant in the thruster plenum chamber was heated up to about 2,OOOK (750s of Isp for hydrogen) by the 10m diameter big concentrator of Tohoku Univ. of very precise paraboloidal shape. But it was difficult to measure the very small thrust under the very high temperature and vacuum condition.

Original language	English
DOIs	https://doi.org/10.2514/6.2001-3733
Publication status	Published - 2001
Event	37th Joint Propulsion Conference and Exhibit 2001 - Salt Lake City, UT, United States Duration: 2001 Jul 8 → 2001 Jul 11

Conference

Conference	37th Joint Propulsion Conference and Exhibit 2001
Country	United States
City	Salt Lake City, UT
Period	01/7/8 → 01/7/11

ASJC Scopus subject areas

Energy Engineering and Power Technology
Aerospace Engineering
Control and Systems Engineering
Electrical and Electronic Engineering
Mechanical Engineering

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50mm cavity diameter solar thermal thruster made of single crystal molybdenum. / Shimizu, Morio; Naito, Hitoshi; Sahara, Hironori; Fujii, Tadayuki; Yugami, Hiroo; Okamoto, Ken Ichi; Takaoka, Shigehiko.

2001. Paper presented at 37th Joint Propulsion Conference and Exhibit 2001, Salt Lake City, UT, United States.

Research output: Contribution to conference › Paper › peer-review

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abstract = "This paper shows design, fabrication and experimental results of a large (50mm) cavity diameter windowless type of solar thermal propulsion (STP) thruster made of single crystal molybdenum (SCM) with tungsten chemical vapor deposition (W-CVD) coating. The nitrogen or helium propellant in the thruster plenum chamber was heated up to about 2,OOOK (750s of Isp for hydrogen) by the 10m diameter big concentrator of Tohoku Univ. of very precise paraboloidal shape. But it was difficult to measure the very small thrust under the very high temperature and vacuum condition.",

author = "Morio Shimizu and Hitoshi Naito and Hironori Sahara and Tadayuki Fujii and Hiroo Yugami and Okamoto, {Ken Ichi} and Shigehiko Takaoka",

year = "2001",

doi = "10.2514/6.2001-3733",

language = "English",

note = "37th Joint Propulsion Conference and Exhibit 2001 ; Conference date: 08-07-2001 Through 11-07-2001",

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AU - Shimizu, Morio

AU - Naito, Hitoshi

AU - Sahara, Hironori

AU - Fujii, Tadayuki

AU - Yugami, Hiroo

AU - Okamoto, Ken Ichi

AU - Takaoka, Shigehiko

PY - 2001

Y1 - 2001

N2 - This paper shows design, fabrication and experimental results of a large (50mm) cavity diameter windowless type of solar thermal propulsion (STP) thruster made of single crystal molybdenum (SCM) with tungsten chemical vapor deposition (W-CVD) coating. The nitrogen or helium propellant in the thruster plenum chamber was heated up to about 2,OOOK (750s of Isp for hydrogen) by the 10m diameter big concentrator of Tohoku Univ. of very precise paraboloidal shape. But it was difficult to measure the very small thrust under the very high temperature and vacuum condition.

AB - This paper shows design, fabrication and experimental results of a large (50mm) cavity diameter windowless type of solar thermal propulsion (STP) thruster made of single crystal molybdenum (SCM) with tungsten chemical vapor deposition (W-CVD) coating. The nitrogen or helium propellant in the thruster plenum chamber was heated up to about 2,OOOK (750s of Isp for hydrogen) by the 10m diameter big concentrator of Tohoku Univ. of very precise paraboloidal shape. But it was difficult to measure the very small thrust under the very high temperature and vacuum condition.

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T2 - 37th Joint Propulsion Conference and Exhibit 2001

Y2 - 8 July 2001 through 11 July 2001

ER -

50mm cavity diameter solar thermal thruster made of single crystal molybdenum

Abstract

Conference

ASJC Scopus subject areas

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